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Beckett AFII 150 Burner User Manual

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1. 25 1 60 r 6 20 MAX FIGURE 2 2 MK VI MK VIII EGPWS OUTLINE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 44 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 30 MAX 4 PL MK VI MK VIII EGPWS MOUNTING TRAY FIGURE 2 3 Proprietary notice on title page applies DWG 060 4314 150 REV SHEET 45 CAGE CODE 97896 SCALE NONE SIZE Honeywell MK VI MK VIII EGPWS Installation Design Guide THIS PAGE INTENTIONALLY LEFT BLANK Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 46 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION Ill SYSTEM PLANNING Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 47 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION III SYSTEM PLANNING SECTION III SYSTEM PLANNINGCG 3 IINTRODUGTION arit ni enn TO t tes 3 2 SYSTEM W RING ELECTRICAL INTERFACES aaa teen nennen nennen nenne nentes nennen 3 2 E Pri
2. 1 60 MAX d 5 04 6 20 1 FIGURE 3 3 1 OUTLINE DRAWING FOR THE MK VI AND MK VIII EGPWC Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 162 Honeywell MK VI MK VIII EGPWS Installation Design Guide e x gt m 4 PL FIGURE 3 3 2 MOUNTING RACK FOR THE VI AND MK VIII EGPWC Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 163 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 ELECTRICAL INTERFACE 4 1 Introduction The MK VI and MK VIII EGPWS provide electrical interfaces for aircraft systems and to support maintenance functions The interfaces are made via the front panel aircraft interface connectors front panel maintenance test port and front panel LED s A TNC coaxial connector is located on the front panel for internal GPS receivers in the 965 1190 0XX MK VI EGPWC and 965 1220 0XX MK VIII EGPWC only The following sections describe the types of electrical interfaces provided in the EGPWC See Section 5 for the specific interface configuration capabilities of the MK VI and MK VIII EGPWS 4 2 Signal Interfaces This section identifies and describes the number and characteristics of each interface type provided in the
3. jenas geq jeues q 9 1 9 E M3TIOHLINOO 82 S34 9 9 1431 HJTIOHINOO AV 1dSIG LH9I L8 Lb8 0G DWG NO 060 4314 150 REV SHEET 86 SCALE NONE SIZE A Proprietary notice on title page applies CAGE CODE 97896 Honeywell MK VI MK VIII EGPWS Installation Design Guide Ov9 CAW Ies1e tuf Ov9 C4W Aq lqeinBiJuoo X0 L XXXI 0r9 wyo oZ V O9pIA g U JoUOD ejdsiq V g V 0v9 CSIN 20 06 76 uopejesuj Adesig 4 SolUOIAY ees 0 9 24 jo uonesado pue 104 uonov sng duie1 Agz 1591 dwe g V INO Z O9PIA HdO M g V INO L O9PIA g V INO 103009 ONIHV g V zit ONIHV g V ul ONINV SMd93 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 87 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 9 Category 7 Options Select Group 1 Category 7 enables disables the following Options Steep Approach TA amp D Alternate Pop Up Peaks Mode Obstacle Awareness Bank Angle Flap R
4. 453 1 1 59 7 2 Display Input Control Group 248 CHANNEL CONNECT TO IC600 1 FDR Bus Fault Designation FDR BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 36 Range 6 2 23 050 Bits 11 14 2000NM Basic N A 100 Discrete Word 6 2 28 275 Bit 17 Discrete Basic N A 500 CHANNEL CONNECT TO IC600 2 FDR Bus Fault Designation FDR BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range 6 2 23 050 Bits 11 14 2000NM Basic N A 100 Discrete Word 6 2 28 275 Bit 17 Discrete Basic N A 500 Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x and 7 1 6 x 2 42 Integration Notes The EGPWS ARINC 429 Output Bus must be connected to the display Display channels 1 and 2 are multiplexed on ARINC 453 Bus 1 The Terrain display will Pop Up in response to EGP WS label 274 bit 28 Left display and bit 29 right display The system has only one range for terrain display on MFD therefore the range to use depends on the value of label 275 bit 17 5 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This
5. Sector Scan used for bolt on EDZ displays only 6 5 2 Honeywell RS 232 Serial Control Interface for DC811 Up Down Range The DC811 controller transmits a 6 byte data packet with spacing between bytes of 16 67 mSec Each byte consists of one start bit low 8 data bits with least significant bit LSB first an EVEN parity bit and one stop bit high The LSB of the first packet byte is set to 1 to indicate the start of the packet the other 5 bytes will have the LSB set to 0 The data rate for this bus is 7 8125 KBS 0 01 Depressing the Up or Down Range button will cause an Up or Down Range bit to be set for 1 packet period approximately 100 mSec After an Up or Down transition no additional changes will be allowed for approximately second EGPWS Up Down Ranges Supported DC811 Data Packet in Nautical Miles BYTE BIT DESCRIPTION 2 5 1 0 1 Start of packet flag 5 2 10 3 25 4 6 1 increment 50 5 1 Range decrement 100 6 default on power up Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 296 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 6 Discrete Inputs This section contains a brief description of each input discrete is used in the EGPWS There are 28 possible discrete inputs each have one of the following input characteristics 1 15 Open Ground two
6. 52 222222 ee sre etes eme ee 52 3 2 4 Analog d Digital Inputs h a a auu dete alie ie tete nont 52 AP UD ICI 52 3 26 Serial ree t tee tte rire 52 32 T Audio Wp 53 32 0 D e nie au enm ene 53 3 2 9 Configuration Module ree 53 3 3 CATEGORY 1 AIRCRAFT MODE SELECT 54 3 34 Aircraft Mode Type eo cem shies aed ah dg dated ea ld td dec 54 3 32 Mode T type s A ed ed 54 3 33 Ro OP 54 334 Mode J tyDe e tee e 55 3 35 Mode V types ii et denies 55 3 36 Bank Angle Type ie e th e Ce e erae iie bea ben d 55 3 3 7 Runway Length MK VIII EGPWS 56 Si SOMHSEEUCHORS us u 56 3 4 CATEGORY 2 AIR DATA INPUT SELECT ent EEEE AE E EAEEREN EAST EN 57 34 Analog Cat 2 1D 0 3 2 TE 42 tee n a 57 242 D
7. P901 T P901 k only NOTE 2 51RV A only Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering ePlease contact the manufacturer s customer service to confirm your installation 1 066 1078 00 01 04 05 10 11 14 and 15 only SHEET 95 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 11 6 Digital Glid eslope Localizer ILS Select Interface Cat 9 ID 2 3 4 EGPWS MK VI MK VIII J2 ILS 429 Bus ON ARINC 429 is IX ARINC 429 B 5 5 I B Low Speed Digital ILS vsd Vendor Model Cat 9 ARINC 429 Bus 1 ARINC 429 Bus 2 ID A B A B Honeywell KNR 634A 2 3 P6342 41 P6342 42 P6342 44 P6342 45 Chelton VNS 411A 2 3 P1 C P1 D Chelton VNS 411B 2 3 P1001 62 P1001 103 Honeywell RNA 34A 2 3 P1024 24 P1024 28 P1024 21 P1024 25 Honeywell 40 4 401 403 41 401 403 42 401 403 44 401 403 45 Collins VIR 432 2 3 P1 35 P1 36 P1 22 P1 23 Garmin GNS 430 2 3 P4006 24 P4006 23 NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation 3 11 7 Digital ARINC 429 Dual buses Cat
8. 113 Jl OI aun E rre t e ede ele pase ee 113 3 17 CATEGORY 15 17 UNDEFINED INPUT SELECTS esses aaa pamahalaan aska lui 114 35174 Undefined Input Select eet do cete ate E ae ore eMe eas 114 34172 Instr cliohsu caet m decet hig Lone 114 SECTION IV CONFIG MODULE PROGRAMMING AND REGIONAL LOADING 117 ett P eL em 117 4 2 HARNESS CHECKOUT AND POWER 117 AS UNEP INSTALLATION onte hom ete a b eam te i eot us 117 4 4 EGPWC INITIALIZATION AND innen innen 117 4 4 1 RS 232 Communication with the MK VI VIII EGPWS sesenta 117 4 4 2 EGPWC Front Panel Test Connector 118 4 43 119 4414 WinVIEWS ODperation uya rt mite edt reete rette eerte le eet ree ite t 119 4 5 CONFIGURATION MODULE treni nne eren 119 45 1 CUW and CMR Commands iu e eau ae ecd ded do este de ud aed ee te 121 4 5 2 Configuration Module Reprogrammi ng 122 4 6 TERRAIN DATABASE LOADING eiin rer tere Re Ope p Her ere eT HR DER AUG 122 2 61 Effeetivily eiie diede eene tate d
9. 90 3 10 CATEGORY 8 RADIO ALTITUDE INPUT 5 91 3 10 T Radio Altitude Input aae nee h ToT ALA aa ela eee eed 91 3 10 2 Decision Height Discrete Input vsti n uod ed ABE d de e ee 91 3 10 3 Digital Radio Altitude Interface 8102 91 3 10 4 Analog Radio Altitude Interface Cat 8 ID 0 1 3 4 sse 92 3 10 5 Digital ARINC 429 Dual IOC Buses Cat 8 ID 251 255 a eee 92 3 10 60 ee e ONG der ee NE UR HORE Pe Eee e AUR NE dh Lae Vind E ER PAR TERES 95 3 11 CATEGORY 9 NAVIGATION INPUTS 2 94 3 11 1 Navigation Inputs Select Glideslope amp Localizer Inputs 94 3412 Glideslope Validity e d eet a rite cete rae Recte oou odere tee 94 31 3 Localizer Validily eta dete re e eter er eere ied tentes 94 3 11 4 ILS Tuned Discrete Input 1 28V and 2 sse emen 94 3 11 5 Analog Glideslope Interface Cat 9 ID 0 1 5 95 3 11 6 Digital Glideslope Localizer ILS Select Interface Cat 910234 96 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 7 Honeywell VI MK VIII EGPWS Installation Design Guide 3 11 7 Digital ARINC 429 Dual IOC buses Cat 9 ID 250 255 a ene 96
10. NO NO NO Un Un Un CA CA Notes y Slowest acceptable update rate in milliseconds This label is not required Data used if present Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 189 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 3 10 Position Input Type 10 Low Speed ARINC 743A GPS no N S E W Velocities CHANNEL CONNECT TO GPS ARINC 743A Fault Designation GPS BUS 429RX 4 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 1000 Altitude 6 2 4 131 072 FT Basic 0 125 1000 VFOM 6 2 13 32768 ft Basic 0 125 1000 HFOM 6 2 10 16 Basic 0 000061035 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125 1000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 1000 Sensor Status 6 2 16 Discrete Wd Basic n a 1000 UTC 6 2 17 Discrete Wd Basic 0 1 min 1000 Date 6 2 18 Discrete Wd Basic 1 day 1000 Notes Slowest acceptable update rate in milliseconds This label is not required Data used if present Table 5 3 3 11 Position Input Type 11 Low Speed ARINC 743 GPS no N S E W Velocities CHANNEL CONNECT TO GPS ARINC 743 Fault Designation
11. D n LNeNl 227 E 1ndinp 31300510 dfid d 51 2931 8459 2 9190 9190 1ndinn 914510 NIVAJIL Y 57 6 m H TWNIWON SHHO 8 108100 309245 73 31 2 P cd 207 3sannoxoeg NO 20 511 Zura f SIS TRAD 07 NOIS oc Rar MIS 9 2 ALIGET 82 s o 123 3s 30 0393 571 ono od 5 9 51 INI INdNI 5576 5 38 d 21182510 i 5 9 HS 8r L Ap i oe d 01190 S3WDISn2 n HOLIMS OINGIAV Q9 A30 O01 TUN A33 832179011 3Sanuox2va UN Nd 1812 MIT 113 12 114 UND 735 SH TUN 711 IND 738 ST 2UN 6 190 5 9 5 2 341530119 La 21 WNBIS 7 6 a 22 14942419 j 2 s 19 Fae ly 09 day Ob 0 SAd5 Nd 338 172 Y4 30 5 0 17003 1 23 3415319 uazrivoo1 5 v HI 179 ave 119 098 ala m IH LINN 1 8 09 sna 553 82 LivNOMIV
12. EGPWS MK VI MK VII J2 Buses 5 ARINC 429 AJ 97 M High Speed IOC Bus 1 L B 36 F ARINC 429 J 41 M High Speed 1 LB 40 F ARINC429 IOC vsd Cat 2 IOC Bus 1 IOC Bus 2 Vendor Model ID A B A B BD 100 255 A4P1 1 4 1 2 4 101 1 4 101 2 CJ 1 CJ 2 255 P1 1 P1 2 P101 1 P101 2 NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation 3 4 6 Instructions Using Appendix E Tables 5 2 5 3 2 and 5 3 2 x as described above select the Air Data Type that matches the aircraft air data configuration feature preferences and version part number being installed Record the ID number for the Air Data Type from Appendix E Table 5 3 2 under the Ident No heading for Step Category 2 in Appendix E Table 5 2 Using the Air Data Type number from Appendix E Table 5 3 2 as x go the Air Data Input Select Table The electrical interfaces pin outs for the Air Data Input Select are shown in Appendix E Table 5 3 2 and are used to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 62 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 5 Category 3 Position Input Select Category 3 defines the Global Position System bus type and interface The
13. IO CA 2 9 9 9 8 5 9 2 amp 5 9 C3 2 5 2 2 5 MOOOMIOOOO Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 323 Honeywell MK VI MK VIII EGPWS Installation Design Guide 9 DEFINITIONS The following acronyms are provided for use with this document Acronym Interpretation AAAS Alternate Audio Alert Select ADC Air Data Computer ADS Air Data System AGC Automatic Gain Control AGL Above Ground Level AHRS Attitude Heading Reference System AIC Analog Input Controller AIMS Airplane Information Management System ASA AlliedSignal Aerospace AOA Angle of Attack ASL Above Sea Level ATP Acceptance Test Procedure BCD Binary Coded Decimal BIST Built in Self Test BIT Built In Test BITE Built In Test Equipment BNR Binary C O Callouts CAA Civil Aviation Authority CAIMS Central Aircraft Information Maintenance System CFDS Centralized Fault Display System CFIT Controlled Flight Into Terrain CFM Cubic Feet per Minute CISRD CFDS Interface System Requirements Document CMC Central Maintenance Computer COTS Commercial Off the Shelf CP Control Panel CRS Course CW Clockwise DAA Digital Analog Adapter DADC Digital Air Data Computer DAU Data Acquisitio
14. Anytime 20 Manual deselect Anytime Auto Range N 11 Moving Marker _ No Overlay Page Without Peaks TERR located at the bottom left of display With Peaks Peaks numbers located at the bottom left of display Display bus type ARINC 453 DISPLAY BUS 1 CONNECT TO 453 1 1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 222 22 142 DISPLAY BUS 72 CONNECT TO NUMEN EE gt J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 Bon s 7 er Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic 12 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B 2 40 Range Display Word 2 2 20 271 Discrete 5 320NM Basic N A 100 Auto Pop Up Category 7 Options Select Group 1 J1 32 GND DISC 12 au Display Select Discrete 1 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal O
15. Data Reference Sig Bits Range Signal Type Resolution Rate ms Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 Discrete Word 6 2 55 Discrete N A Basic N A 200 CHANNEL CONNECT TO KCPB IND Bus 2 out Fault Designation KCPB BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms 12 41 Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 B J2 40 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 Discrete Word 6 2 55 Discrete N A Basic N A 200 Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed 12 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x J2 42 Integration Notes 1 When interfacing to a single display controller configuration the Display Input bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 KCPB Keyed Component Picture Bus is also known as ASPB AlliedSignal Picture Bus 3 Label 012 is optional The current fault and fault history message RANGE for label 271 Range is not shown if Range Ke
16. due 159 sng SMd93 ano 2 Aejdsig y CH O9PIA ESV ONIHV ul Aejdsiq ureue g cit ONINV V g ls ONINV V ul osjes Aejdsiq ureue g V L O9PIA Sr ONIHV ano 2 Aejdsig Proprietary notice on title page applies CAGE CODE 97896 DWG 060 4314 150 REV SHEET 83 SCALE NONE SIZE A HONEYWELL MK VI VIII EGPWS 965 1XXX OXX RANGE INPUT A RANGE INPUT B RANGE INPUT A RANGE INPUT B MOM TERR SELECT 1 ARINC 453 OUTPUT A ARINC 453 OUTPUT B TERR RLY SELECT 1 MOM TERR SELECT 2 ARINC 453 OUTPUT A ARINC 453 OUTPUT B TERR RLY SELECT 2 J2 Honeywell MK VI MK VIII EGPWS Installation Design Guide PROLINE 4 INTERFACE MK VI VIII EGPWS Category 6 ID 5 or 6 1 IOC ICC 4000 37 36 41 40 P1 CC 851A pins 13 amp 14 LA GP 5 bus Label 271 2 IOC ICC 4000 CC 851A pins 13 amp 14 RA GP 5 bus Label 271 J1 n the OEM installations a single weather radar 453 bus enters the left MFD passes through and is I i terminated 70 ohm at the right MFD For EGPWS TERR installations break the 453 radar bus between the BN MFDs install switching relays and wire one relay to each MFD The right MFD connection is moved to 3
17. 6 5 CANCLD B GPWS FLAP OVRD GPWS INOP G S CANCLD switch annunciator assemblies The GPWS FLAP OVRD annunciator provides visual indication that the EGPWS Flap Override function is activated The GPWS FLAP OVRD annunciator also has a momentary switch that is used to manually activate the Flap Override function The GPWS INOP annunciator provides visual indication that the EGPWS GPWS modes have been disabled or do not function because of an external or internal fault The G S CANCLD annunciator provides visual indication that the EGPWS Mode 5 function is inhibited Vendor Name Vendor P N Description QTY UM West Coast Spec 90 81401 008 1 1 EA West Coast Spec 90 81401 009 2 1 EA West Coast Spec 90 81401 010 3 1 EA Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 22 Honeywell MK VI MK VIII EGPWS Installation Design Guide West Coast Spec 90 81401 011 4 1 EA West Coast Spec 90 81401 012 5 1 EA STACO 61406 007 GPWS FLAP OVERRIDE 1 EA 1 GPWS BELOW G S GPWS FLAP OVRD G S CANCLD 2 GPWS BELOW 5 GPWS FLAP OVRD GPWS INOP gt GPWS G S CANCLD GPWS FLAP OVRD GPWS FLAP OVRD GPWS INOP 3 GPWS FLAP OVRD G S CANCLD 5 C TERR DISPLAY TERR INHIBIT GPWS FAIL TERR FAIL switch annunciator assemblies The TERR DISPLAY annunciator provides visual indication that t
18. gM euoH pSA 000LSnuiiq 0002102 3409 SMd94 009 21 1e3nduio2 SOIUOIAY pojeJ6oju OOEVLOZ ul sng G s fe Cu V Y 028 eldsiq 00 vL0A ul sng 028 yun ejdsiq 0004104 g cv 009 21 49 nduioo SOIUOIAY 40 020 0 21 996 MIN aadal ZL ul 1qtuuj jse duie1 g INO J0 8Jeuoec y 194 6 esr ONIHY ul zit ONINV INO sng Iolluoo ONIYV g V Ul ONINV SMd94 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 77 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide V 8LNI 0002 xipu g sng duie1 Agz 1591 due1 um sng YMd SMd93 A82 9 Xx v90 990 V 8LNI L HO UO LE sng q 1 y sng Ionuoo 0000 7900 900 enuey uonejejsu jewKeuoH JeuyeeM 10 09 0002 eu Jo uoneJedo pue 103 uonoy C DH c 0002 LYV Ij9M ouoH J8je JO 020 0 21 996 IIIA J8j8 JO 020 0X 01 496 IA ino dONI ureue p ureue ino
19. lt See __ Spe Spare Lamp Output lt 28vdisc Attitude Validity Discrete 28VDC TCAS inhibtOutput Ou X Lampout gt gnd AwioONOupt OOo Audio Speaker Output B ohm H Output X HL Audio Out H gt HighlevelAudicOutput B AudioSpeakerOuput amp ohm L Outpt X JT gt HighlevelAudioOutput BQ GPWS System Status Lamp _ Output X JZ Monitor Out gt gnd GPWSINOP monitor Faillnoplamp GPWSFapOVRD X 042 Lampout gt and Wishes Wang i Auioiowlewi X 0 gt Low Level Audio udio tow Leve Ow X Jt Low Level Audio 600 ohm H Giideslope Canceled Lamp X 476 Lampout gt ond GldesiopeCancelOutput te GS CANCL D Temp GPWS Warning Output to red GPWS or Pull Lamp GPWS Alert Warning Lamp X J1 78 Lampout gt Terrain Caution or Warning Obstacle Caution or Warning Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 133 Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name GPWS 965 0686 001 020 Signal Type i m Signal Name MK VI MK VIII EGPWS Enhanced NEW CONNECTOR ILSARINC 429 Input Ble 2w GPS
20. L 0 w T 2 _ 1 o 0 o G 9UNM _ 1 0 _ 1 1 T se Note The range bits are additive 2 if bits 24 and 26 1 then the range would be 25 6 2 20 1 Control Word 2 271 273 Type 2 DISPLAY WD 1 NAV DISPLAY BUS For FDS 255 display the label is 273 Data Bits Discrete word see below Sign Bit N A Pad Bits 9 10 Transmit Interval mSec 100 ms Data Type Discrete SDI Bits N A Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 281 Honeywell MK VI MK VIII EGPWS Installation Design Guide CONTROL WORD 2 BIT ASSIGNMENTS Bit No DEFINITION 11 22 Spares Display Range Divide by 20 24 29 Display Range as specified in the table below BITS 24 to 29 Display Range 5 to 320NM format as follows 0 1 SNM 0 0 o o T 0 1 20NM p 1 40NM 0 1 0 0 0 0 80 PF i 10NM Note The range bits additive 2 if bits 24 and 26 1 then the range would be 25 6 2 21 Discrete Word 155 or 176 MFD DISCRETE WORD MFD Source MFD or IOC 1 amp IOC 2 Approx LSB N A Sign B
21. 060 4314 150 REV SHEET 18 Honeywell MK VI MK VIII EGPWS Installation Design Guide The MK VI EGPWS is normally shipped with an AMERICAS Terrain database When ordering a MK VI EGPWS that will be operating in the ATLANTIC or PACIFIC region the specific Terrain database must be specified with the order NOTE 1 Terrain Database cards for the ATLANTIC or PACIFIC region are no longer required to be ordered separately NOTE 2 XXX defines Application software version 1 7 2 MK VIII EGP WS The MK VIII EGPWS is available two versions with internal GPS card or without The part number for the units is as follows 965 1210 without internal GPS card 965 1220 XXX with Internal GPS card The MK VIII EGPWS is shipped with a world Terrain database NOTE 1 XXX defines Application software version 1 7 3 Configuration Module The MK VI MK VIII EGPWS Configuration Module is available in two versions When ordering the Configuration Module order part number 700 1710 020 or part number 700 1710 001 The part number 700 1710 020 is required for installations with internal GPS 1 7 4 Smart Cable PCMCIA Interface The MK VI MK VIII EGPWS Smart Cable is available in one version The Smart Cable is used for Line Maintenance Application Configuration code and Terrain Database uploads and Flight History downloads Only one Smart Cable is required for an installation house or operator When ordering the Smart Cable order part number
22. Kejdsiq ul 3oejes Aejdsig INO Z Sr ONISV INO ESV ONISV V ul z ONINV g V u Li ONINV SMd93 Proprietary notice on title page applies CAGE CODE 97896 DWG 060 4314 150 REV SHEET 78 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide xipueg Pps arvrldd sng duie1 A8Z 1591 dwe sng HMd SMd93 A82 O XXXX CCCL VOC St ldd L HO UO SL y sng Jojeoipu XYM 4938 JO 020 0X2 1 896 IIIA JO 020 0X L L S96 IA dONI ino Aeldsig g V INO Z O9PIA ESP ONIYV g V INO L O9PIA ONIHV g V zit ONINV g V ONINV SMd93 Proprietary notice on title page applies CAGE CODE 97896 DWG 060 4314 150 SHEET 79 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide 599 WNHYALNIIM SMd93 IIIA 020 022 996 SMd93 IIIA XHVIN 020 021 596 Sd9 1 1 SMd93 IA MYWW 020 061 296 SMd93 IA XHVIN 020 081 1 596 SH38IAQN LYYd YALNdWOD SMd93 OL GALNOddNS LON SI NOLLVHOOIJNOO SIHL ir NOLLV
23. meum c I i Bizjet Turbofan default GPWS modes with Bizjet Bank Angle Callout and 3500 ft and greater runway database N A MK VIII Only Note 1 Bizjet Turbofan default GPWS modes with Bizjet Bank Angle Callout and 2000 ft and greater runway database MKVIII Only Note 1 ID 254 is supported with terrain database 426 and later Aircraft Model Mode2 Mode3 Mode4 SA Fast 4 4 2 6 4 GA Fas 4 4 2 s 4 1299 FHR GA Fast Fast Turboprop Slow Turbofan 4 Bizet See Product Specification 965 1180 601 for a description of Mode X type number Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 178 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 2 Category 2 Air Data Input Select The following table provides identification of the Air Data source type The entry in the Air Data Type corresponds to a table that provides detailed information on the configuration For example the details for Air Data Type 2 are found in Table 5 3 2 2 In this category only the following signals are defined e Uncorrected Barometric Altitude in analog ARINC 575 or ARINC 429 format and associated validity Temperature Outside Air or Static Air in analog ARINC 575 or ARINC 429 format Corrected Barometric Altitude in ARINC 429 format Barometric Rate in ARINC 575 or ARINC 4
24. sss m Smear MON_OUT_1 GPWS INOP Discrete TAD INOP Discrete GPWS Warning Discrete J1 78 DISC_OUT_1 Output Terrain Awareness Caution or Warning Obstacle Awareness Caution or Warning 550 0 2 oupa GPWS Alen Discrete Gldesione 0 DISC_OUT_3 Glideslope Cancel Discrete Output Flap Overide Discrete oo o Oww Terrain Awareness Caution or Warnin DISC OUT 9 TemaDispaySelect2Discete 74 0 J148 28V DISC 11 input NotDefnedinthisID Note3 o Cd J215 28V DISC 13 Input NotDefinedinthisID Note3 To Cd J150 MONOUTS3 Output _ Not Defined in this ID Note 3 J1 52 DISC_OUT 7 Output Not Defined in this ID Note 3 Configuration Data Possible States Type 1 2 1 Flashing Lamps Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word bit if configured by the display type Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 259 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 1 Input Output Discrete Type 1
25. 46 Dn GS Valid 28 11 Super Flag 28V Low Level 30 X GS Flag GS Valid 49 e Low Level ILS 28 39 Delayed ILS Mode Tuned GND 20 ILS Energize ui 30 S LOC Deviation L LOC Deviation 10 N Z R LOC Valid 28 48 LOC Val 28V GS Inhibit BC 28 38 Backcourse GS Inhibit BC GND 19 Backcourse Analog ILS 1 vsd GS Valid LOC Valid ILS Tuned Deviation Cat 9 SuperFlag Low Level SuperFlag GS up LOC R ID 28V dn L Honeywell J1003 21 J1003 8 J1002 39 KNR 6030 5 51003 27 J1003 22 71992 50 41002 18 4400239 1002 40 Honeywell 4 P1 e 1 KNR 660 P1 q k P1 V Honeywell P6342 34 P6342 36 P6342 23 KNR 634 5 P6342 50 pe342 18 6342 49 P6341 17 p6342 35 P6342 7 Honeywell P692 S P692 B 691 0 P692W 2 692 692 Honeywell 601 601 601 KNR 600A P601 q P601 A HOOK P601 s P601 n Collins 5 21 8 39 51RV 1 51RV 4 12 TP 22 BP 50 Bro TP 9 BP 40 Collins P1 9 P1 5 P2 10 VIR 30 31 32 3e 1 13 anis P240 P1 1 P2 13 Honeywell J1001 90 J1001 38 VNS ATA 5 P1001 60 P1001 101 21001 56 40023 1001 02 Honeywell TP 8 BP 39 B 5 TP27 TP 21 BP 50 BP 18 Dis 55 Honeywell P2 13 P2 P KN 53 P2 R P2 12 2 14 Honeywell P1 2 KN 72 P1 10 Honeywell P1 B60 P1 B79 P1 B78 RNZ 850 5 P1 A 4 1 106 P1 8 1 1 64 P1 B75 P1 B75 Honeywell P901 U P901 S P901 s KX 165 KX 155 165 P901 R
26. Anytime WXR ison and display isinproperMode r Manual deselect Any me Auto Range 1 Moving DNE __ _________ __ __ _ M 5 Overlay Page Yes TERR or Peaks Elevation located on upper right side of Terrain image 1 5 5008 453 1 B J1 59 72 453 2 B J1 57 72 Display Input Control Group 2 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM Basic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution A J2 41 Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A B J2 40 Range Display Word 2 6 2 20 Discrete 5 320NM Basic Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CONNPIN REFERENCENAME PINFUNCTION Peolarity Configuratin J1 32 GND DISC 12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Referenc
27. Down Above Beam Fly Down 1 gt 83 lt 200 LA 0 to 2500 feet 37 7V 2 Vra 2 2 5V 29 7V gt Vc 2 0 4V 0 1 Second Low Pass 10 Input will be biased to less than 50 feet J1 64 RALT H J1 45 RALT L 1 gt 2 5 lt 6 2 uA 12 Dots 0 9 VDC 0 1 Second Low Pass 10 Differential 11V Vem 2 2V Input will be biased less than 15 dots 11 65 GSDEV_H 11 46 GSDEV L 4 2 3 3 Localizer Deviation or Low Level Glideslope Validity This input can be configured as either a low level glideslope valid or as a localizer deviation input Installations that only have the low level validity signal for glideslope can not activate the analog localizer input See section 5 3 9 for more information Quantity Input Impedance each leg Reverse Fault Current Input Filter Input Type Common Mode Voltage Range When used as a validity input Pin Assignment Signal Mnemonic Flag Flag Active Voltage Range Logic True Inactive Voltage Range Logic False Broken Wire Detect When used as a localizer input Pin Assignment Signal Mnemonic CRS DEV Fly Right CRS DEV Fly Left Signal Range Input Voltage Range Broken Wire Detect Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A 1 gt 2 5 lt 6 2 uA 0 1 Second Low Pass 10 Differential 11V gt Vom 2 2V J1 30 GS_VAL_H 10 GS VAL 1 160 to 840 mVDC 0 to 50 mVDC Inp
28. Proprietary notice title page applies SHEET 142 DWG 060 4314 150 REV SCALE NONE SIZE A CAGE CODE 97896 Honeywell MK VI MK VIII EGPWS Installation Design Guide Y y STE ANA 1 A c IV Jano Pd em HS M m dd 7 X SM J Sa ae LI IHNI 87 69 1ND lI8IHNI S diu 133HS I8LA WveOvId DNISI A Wa BI SNE Q9 438 WA 9 Ee 8 1 82 31340510 f TWA ONIGWIH 8 1 pn Se SSR OS ONIY gt 4 NU div ND dD a Ov Jj 2 Id arwa B elf FOND rS AND 2l 338 v S Hv 9A TUN 12 woo er SNIGV3H OIL3NOVW 3Gn LLLLV ONL ma N9 123135 3 1 ef 9 31390510 _ 7
29. 060 4314 150 REV SHEET 265 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 7 Input Output Discrete Type 7 CHANNEL CONN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE coer sss umm cgo mem BENI TANTUM TII E o owu GPWS Warning Discrete 741 J1 78 DISC_OUT_1 Output Terrain Awareness Warning 747 2 Obstacle Awareness Warning J1 77 DISC_OUT_2 Output Terrain Awareness Caution 747 1 Obstacle Awareness Caution DScOUrs Ou C 7 Dicour4 Output Flap Overide Discrete ________ y y oisc_our_s ou aoon e msc oore ouput Teran Display 744 Dicour9 Terrain Display Select 2Discrte a J1 52 DISC_OUT_7 Output Steep Approach Discrete TAM os J1 48 28V DISC 11 Not Defined in this ID Note 3 e J2 15 28V DISC 13 Not Defined in this ID Note 3 l J1 50 MON OUT 3 Output Not Defined in this ID Note 3 O w Configuration Data Possible States 1 2 2 Flashing Lamps Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the
30. 4 IERAINAWARENESSINP Lo 7 __ TERRAIN AWARENESS NOT AVAILABLE NOTE Bits 15 17 21 and 29 will be set to zero when Not Supported Bits 15 17 amp 18 are supported by MK VIII EGPWS only provided that WS is included in configuration Bits 20 amp 21 are Not supported 7 1 1 6 EGPWC Alert Discrete 3 300 26 NOTE Bits 15 and 19 27 will be set to zero when Not Supported Bit 15 is supported by MKVIII EGPWS only provided that WS is included in configuration Bits 19 27 are Not supported Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 307 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 2 Internal Data Outputs Internal data outputs are only used for test purposes Tables 7 1 2 1 through 7 1 2 6 are available for both MKVI and MKVIII EGP WS Tables 7 1 2 7 through 7 1 2 15 are are only output when the Honeywell Windshear Algorithm is enabled available only on the MK VIII EGP WS and are only used for test purposes 7 1 2 1 Geometric Altitude VFOM 135 LABEL Octal 135 Max Range 32 768 Ft Approx LSB 0 125 Foot Data Bits 11 to 28 18 Sign Bit 29 Pad Bits N A Transmit Interval msec 1000 10 Data Type 2 s Compliment Binary SDI Bits 9 10 7 1 2 2 Terrain Clearance 164 7 1 2 3 Geometric Altitude 261 7 1 2 4 Computed Terrain Clearance 067 LABEL Octal 067 Ma
31. 4 6 6 Verification of the Terrain Database Version Since the EGPWC software verifies the PCMCIA card loading process this verification is to assure the operator installer that the correct Regional Terrain Database version is installed Terrain Database version verification is accomplished with the EGPWS Self Test ST function The ST function may be initiated from the aircraft cockpit with the GPWS Test Switch NOTE Initiation of the cockpit ST function may vary from one aircraft to another For example the ST function may be initiated by pressing the GPWS PULL UP light assembly or by activating a separate ST switch The EGPWS ST function has 6 levels that describe the current condition and configuration of the EGPWS the fault and warning history and the condition of the various inputs To help navigate through the various levels there are 2 cancel functions SHORT CANCEL press and hold the ST button for more than 0 5 seconds but less than 2 seconds and LONG CANCEL press and hold the ST button for more than 2 seconds but less than 8 seconds The Short Cancel and Long Cancel functions operate differently depending upon the ST level To initiate a ST sequence or to continue from level to level the ST button must also be pressed and held for more than 0 5 seconds but less than 2 seconds which is identical to the Short Cancel function Therefore for simplicity the phrase Press ST Button in the verification procedure me
32. Category 13 ID 254 255 must use this method for Flap Override Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 103 Honeywell MK VI MK VIII EGPWS Installation Design Guide Ground seeking Landing Flap discrete active position Flap Reversal Category 7 Flap Discrete J1 18 False True Landing Flap discrete GND Flaps Up Flaps Down Landing Flap Discrete Open or 28V Flaps Down Flaps Cat 13 ID 254 255 only NENNEN Flap Override NORM Open Open Category 13 ID 254 255 must use this method for Flap Override 3 15 1 3 Audio Inhibit Discrete The Audio Inhibit discrete is an optional input but is strongly recommended to maintain audio and visual prioritization When activated this discrete inhibits all audio Ground Proximity and Terrain Awareness Activation of the Audio Inhibit input for more than 60 seconds will result in the All Modes Inhibit fault The Audio Inhibit discrete input can be connected to any or all of the following as applicable to the aircraft configuration the Stall Warning computers this is required for CAA registered aircraft the Predictive Windshear PWS Audio Inhibit output discrete separately labeled guarded cockpit switch the reactive Windshear system if separate from the EGPWS For some existing GPWS installations this discrete may have been tied to the analog Radio A
33. Windshear Input Select Types 253 254 and 255 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 224 225 and 236 For interface description see paragraph 3 4 5 Air Data Type 255 NOTE Windshear is currently available only for Bombardier Challenger 300 airplanes with MK VIII EGPWS installations 3 14 3 Instruction s Using Appendix E Table 5 2 and 5 3 12 as described above select the Windshear Input Select type that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Windshear Input Select from Appendix E Table 5 3 12 under the Ident No heading for Step Category 12 in Appendix E Table 5 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 102 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 15 Category 13 Input Output Discrete Type Select Category 13 defines the input and output discretes not defined as part of any of the other Categories Appendix E Table 5 3 13 defines the Input Output discretes options and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry 3 15 1 Input Discretes The discrete inputs are defined in Appendix E Section 6 6 Additional information for the discretes is provided below Note When there are two discrete pin choices for the same pin function in Appendix E Ta
34. 11 1 Input Type Basic Roll Attitude 21 6 1 15 Fault Designation ROLL FAULT 2 J1 2 Validity Attitude Validity Discrete 1 Reference None REFERENCE Configuration Discrete 1 lt 4 4 Invalid 4 2 7 Table 5 3 10 5 Attitude Input Select Type 5 CHANNEL CONNECT TO AHRS Fault Designation AHRS BUS 429RX_7 Format ARINC 429 High Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 23 Roll Angle 6 2 31 325 14 180 degrees Basic 0 010986328125 10 20 B J2 6 Pitch Angle 6 2 34 324 14 180 degrees Basic 0 010986328125 10 20 Table 5 3 10 6 Attitude Input Select Type 6 CHANNEL CONNECT TO AHRS Fault Designation AHRS BUS 429RX 7 Format ARINC 429 High Speed Bus Type Basic Data Reference Bits Range Signal Type Resolution Rate ms Roll Angle 6 2 31 5180 degrees Basic 0 010986328125 10 20 Pitch Angle 6 2 34 180 degrees Basic 0 010986328125 10 20 Body Roll Rate 6 2 50 128 deg sec Basic 0 01562500 10 20 Body Pitch Rate 6 2 49 128 deg sec Basic 0 01562500 10 20 Inertial Vertical Speed 6 2 56 32 768 Basic 1 0 20 40 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 253 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 10 253 Attitude Input Select Type 253 CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429RX_7 Format ARINC 429 High Speed
35. ANS WUCTIONS SG a ees E EI UE 97 3112 CATEGORY 10 ATTIT DEINPUT SELECT u eiecit du on pir ret 98 3412 1 Roll Angle mU UAEET 98 3 12 2 Analog Pitch amp Roll Angle Synchro Cat 1010020 5 98 3 12 3 Digital Pitch amp Roll Angle ARINC 429 High Speed Cat 10 ID 5 amp 6 sss 99 3 12 4 Digital ARINC 429 Dual IOC buses Cat 10 ID 253 255 22 2 200000000000000 99 312 LM A Too RE 99 3 13 CATEGORY 11 HEADING INPUT SELECT ere DOG goo re OC oret rte 100 3 13 1 Magnetic Heading oa ate te he etie eti der iq 100 3 13 2 Analog Heading Synchro Cat 11 ID 0 sse 100 3 13 3 Digital ARINC 429 AHRS Input Cat 11 ID 2 amp 3 sse 101 3 13 4 Digital ARINC 429 Dual IOC buses Cat 11 ID 254 amp 255 sisse eee 101 9I o IBSIFUCTOHS uu E ta ae tete ete tene ee 101 3 14 CATEGORY 12 WINDSHEAR INPUT SELECT uma eene G kaum eterne eren nee 102 JA No Windshear ui te rr Ne RA e PARE EAE eletto aree ERE eode 102 3 14 2 Dual ARINC 429 BUS Cat 14 ID 253 254 255 nnne nennen nr eren enne 102 Ouid SIBSIVUCIOHS e oet to ease ute e 102 3 15 CA
36. Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 41 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 B J2 40 Decision Height MDA 6 2 62 170 12 14 4096 16384 Basic 1 0 1000 Table 5 3 8 252 Radio Altitude Input Select Type 252 ARINC 429 via dual IOC buses with DH discrete 1 Fault Designation IOC BUS 1 1 Format ARINC 429 High Speed Bus Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 37 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 72 36 Decision Height format 1 6 2 41 370 16 8192 FT Basic 0 125 100 200 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 41 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 B J2 40 Decision Height format 1 6 2 41 370 16 8192 FT Basic 0 125 100 200 Table 5 3 8 253 Radio Altitude Input Select Type 253 ARINC 429 via dual IOC buses with DH discrete CONNECT TO IOC 1 Fault Designation IOC BUS 1 1 Format ARINC 429 High Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms J2 37 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 B J2 36 CONNECT TO IOC 2 Fault Designation IOC BUS 2 3 Format ARINC 429 High
37. FALSE If the display is in normal MFD mode not HSI backup or SG backup AND if label051 bit 11 transitions from 0 to 1 rising edge AND Checklist is not selected on the MFD AND TCAS Auto Pop Up is not occurring The display will change to Map mode The display will energize the Terrain selection relays The display will annunciate TERR The display will change to the range indicated by the EGPWS ARINC 429 label 050 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 228 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 246 Honeywell Bendix EFIS 10 EFS 86 Radar system MK VIII Only Display Configuration Group 246 Function Value Reference section Display Type Bendix EFIS 10 Non Integrated Sweep Type Normal Sweep range 90 degrees Auto Pop Up Peaks Mode 5 3 7 Peaks Off Peaks On Manual select Anytime __ o y y Manual deselect Anytime o Auto Range Moving Marker LE Overlay Page Yes Without Peaks TERR is located at the bottom left of the display With Peaks Peaks numbers are located at the bottom left of the display Display bus type ARINC 453 pe 453 1 J1 59 7 2 fr pasaruspan EMEN 453 2 J1 57 7 2 Display Input Control Group 246 CHANNEL CONNECT TO WX IND 429 Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1
38. REFERENCE NAME PIN FUNCTION Gnd Display Select Toggle J1 32 GND DISC 12 Reference Display Select Discrete 1 42 7 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 display does not use EGPWS ARINC 429 Output Bus 2 display color palette is not compatible with Terrain in the mode Peaks Elevations are outside of the scan area Sector Scan mode Terrain will not be allowed to display in these modes 3 When interfacing to a single display controller configuration the bus must be connected to both EGP WS input channels This prevents the EGP WS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 226 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 245 Honeywell SPZ8000 EDZ806 Integrated with dual SCI range MK VIII Only Display Configuration Group 250 Display Type Honeywell SPZ8000 new style every fourth display line is blanked Sweep Type Honeywell Peaks Mode Category 7 Options Select Group 1 5 3 7 YeslONM
39. Range Basic Basic Signal Type 0 0001953125 0 00009765625 Resolution 33 3 66 6 33 3 66 6 Rate ms 6 2 30 6 2 33 174 173 0 8 DDM 0 4 DDM Basic Basic Table 5 3 9 254 Navigation Inputs Select 254 CONNECT TO IOC 1 Fault Designation IOC BUS 1 Format ARINC 429 High Speed Bus Type Basic Data Glideslope Localizer PFD Mode Select Word Data Glideslope Localizer PFD Mode Select Word Reference Sig Bits Signal Type 0 0001953125 0 00009765625 Resolution 33 3 66 6 33 3 66 6 Rate ms 6 2 30 6 2 33 6 2 44 Reference Fault Designation IOC BUS 2 Bus T 12 12 Discrete pe Basic Sig Bits Basic Basic Basic Signal Type 0 0001953125 0 00009765625 n a Resolution 33 3 66 6 33 3 66 6 250 Rate ms 6 2 30 6 2 33 6 2 44 12 12 Discrete Basic Basic Basic Table 5 3 9 255 Navigation Inputs Select 255 CONNECT TO IOC 1 Format ARINC 429 High Speed Data Glideslope Localizer Data Glideslope Localizer Reference Fault Designation IOC BUS 1 Bus T Label pe Basic 0 0001953125 0 00009765625 n a Resolution 33 3 66 6 33 3 66 6 250 Rate ms 6 2 30 6 2 33 Reference 117 116 Bus T Label Sig Bits 12 12 pe Basic Sig Bits Range 0 8 DDM 0 4 DDM Fault Designation IOC BUS 2 Range Signal Type Basic Basic Signal Type 0 000195
40. SYN 22 SYN 3X SYN 3Y SYN 32 SYN 4X SYN 47 SYN 42 SYN 5X SYN 5Y SYN 52 These inputs accept 400 Hz AC signals and detect the zero crossings of these signals These zero crossings are used to time the conversion and input of AC signals Absolute voltage level of these signals is not measured but it must be within the range specified below Voltage below the specified minimum value may result in intermittent or jittery zero cross detection Timing reference signals are required for input of most AC devices not required for pitch and roll These references can be brought into the appropriate timing reference input or the system can be configured to derive a reference from the signal Timing reference signals are specified for synchro inputs requiring a range greater than 80 degrees Inputs requiring less i e Roll Attitude are configured to derive a reference from the synchro input signal and do not require a separate reference voltage input Quantity Input Impedance Maximum Reverse Fault Current A C Input Signal Frequency Range Maximum Input Voltage Swing differential Maximum Input Voltage Swing ref to Gnd Input Hardware Filtering Minimum Input Voltage Pin Assignment Signal Mnemonic 26V AC Reference 1 H 26V AC Reference 1 C 26V AC Reference 2 H 26V AC Reference 2 C Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A 2 gt 140KQ each line to
41. 1 11 License Re quirements There are no Radio license requirements for the MK VI MK VIII EGPWS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 25 Honeywell MK VI MK VIII EGPWS Installation Design Guide THIS PAGE INTENTIONALLY LEFT BLANK Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 26 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION INSTALLATION Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 27 Honeywell VI MK VIII EGPWS Installation Design Guide SECTION II INSTALLATION SECTION M INSTALLA TION susi Ses EEE SeS REKE EE 29 2 1 INTRODUC MON g 29 2 2 UNPACKING AND INSPECTING THE 29 2 3 EQUIPMENT INSTAEDATION eite e eterne tese ete a u bete A ens 29 2 3 ata tig aab es 29 2 3 2 MK VI MK VIII Computer Location n pap nas k wa hisa ak S hn enne trennt 29 2 3 3 MK MK VIII Computer Installation 30 2 3 4 Configuration Module Location 31 2 3 5 Configuration Module Installation 31 2 3 6 GPS Antenn
42. 11 to 17 Transmit Interval mSec 1000 Maximum Data 2 s Complement Binary SDI Bits 9 10 6 2 60 Longitude Fine 121 GPS 6 2 61 Selected Course 100 IOC 6 2 62 DH MDA Selected 170 DAU Scaling 4096 feet 16384 feet 17 to 28 12 15 028 14 Transmit Interval mSec 1000 Data Type 2 s Complement Binary Discrete SDI Bits 9 10 Note If Signal Displayed bit 13 1 MDA Selected is mapped to bit 14 SSM for this word uses the discrete word format 6 3 Digital Data ARINC 575 ARINC 575 data is very similar to the low speed ARINC 429 data described in the previous sections but is one generation earlier in the aircraft serial data definition As such there is NO SDI Field and the SIGN STATUS Matrix for 2 s Complement Binary data is different and is given below for reference SIGN STATUS Matrix The number of BITS and the meaning of these BITS varies depending on the type of data in the ARINC 575 word 0 0 Pus North East Right To Above 0 1 Fauucwaens 00 j 0 Computed Data NCD 6 3 1 Static Air Temperature 213 STATIC AIR TEMPERATURE Source ARINC 575 ADC LABEL Octal 213 Units Degrees Celsius Max Range 512 Degrees C Approx LSB 0 5 Deeree Data Bits 20 to 29 10 Above ZERO Sign Bit Part of SSM Pad Bits 9 to 19 Transmit Interval mSec 500 Maximum Data 278 Complement Binary SDI Bits N A Proprietary notice on
43. 2 SOS Overlay Page Without Peaks TERR located in the lower right corner With Peaks Peaks numbers located in the lower right corner Display bus type ARINC453 D 7 i i 453TX 1 A J1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 e _ O a O DISPLAY BUS 2 CONNECT TO L a e 1 57 72 Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Display Word 2 6 2 20 271 Discrete 5 320NM Basic N A 100 CONNPIN REFERENCENAME __ PIN FUNCTION GND_DISC_12 Reference Display Select Discrete 1 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 B J2 42 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x Integration Notes 1 When interfacing to a singl
44. 29 TX Transmit Out CM 28 GND RS232 GPS vsd GPS Alt ARINC NS RS 232 Vendor Model Ref 743 743A EW RX TX GND GARMIN GNS430 530 MSL N A Note 3 P4001 56 Chassis Software Version 2 21 KLN 900 MSL N A OK P9002 13 Chassis 066 04034 0104 or 066 04034 0204 KLN 94 MSL N A OK P941 6 Chassis NOTE contact the manufacturer s customer service to confirm your installation 1 The KLN 89 89B 90 90A 90B are not compatible The GNS 430 software mod is also applicable to the GPS 400 and GNC 420 units 3 Check manufacturer for compatibility with North South East West Velocities Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please SHEET 65 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 5 6 Dual ARINC 429 BUS Cat 3 ID 253 amp 255 NOTE If GPS 2 is not installed in the aircraft then use ID 4 or GPS bus 1 must be connected in parallel to both EGPWS GPS input ports NOTE Non lOC aircraft can use ID 253 or 255 to activate dual GPS inputs for redundancy and improved system availability but the interface must have dual High Speed 743A GPS and this cannot be used if using Category 10 ID 5 or Category 11 ID 2 EGPWS MK VI MK VIII J2 ARINC 429 GPS A 25 15A i Annae M M
45. 50 ft VDC Volts 20 ft For Radio Altitude gt 500 feet gt 10 4 VDC Volts 0 003 RALT 500 10 4 or RALT ft 333 3333 ft VDC Volts 2966 7 Reference Dynamic Range ge Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 270 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 1 3 Uncorrected Barometric Altitude Data Item Value Signal Dynamic Range 19 334 to 31 166 Feet Discrete Validity 6 1 4 Outside Air Temperature 500 ohm probe AIC Name D2 DC2 85 to 60 C Voat lt 0 43448 gt 0 43448 and lt 0 49212 gt 0 49212 and lt 0 54816 gt 0 54816 Input Signal Connection _____ 1 63 J1 44 see section 5 3 2 for hookup Input Reference Connection None Input Signal Connection AIC Name D External Validity Flag Connection AIC LSB 0 03125 C AIC Status Mask 0000200F External Validity Type 6 1 5 Outside Air Temperature Internal Constant Data Item Signal Name AIC Algorithm Signal Dynamic Range Signal Reasonable Range Signal Open Wire Threshold Reference Dynamic Range Reference Reasonable Range Scale Input Signal Connection Input Reference Connection AIC Name Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 271 Honeywell MK VI MK VIII EGPWS Inst
46. CDU XLs 0 Low MSL 743A JA A01 JA A02 14141 0624 SM04 HG2021GBXX 15 MSL 743 J1 38 J1 39 J1 24 J1 25 HG2021GC GDXX 0 4 HIL MSL 743A J1 38 J1 39 J1 24 J1 25 HT1000 HT9100 10 12 HL WGS 84 743A 02 01 FreeFlight Trimble 2101 I O Approach Plus 0 Low MSL 743A J1 16 J1 23 J1 58 J1 57 81440 XX software ver 241F NOTE O N The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation The Enhanced GNS XLS ARINC 429 bus also contains Range label HG2021G Pin 21 open high speed Pin 21 GND Low speed GPS 4000 North South Velocity label 166 and East West Velocity label 174 are required in MK VI MK VIII 008 software and on NOT COMPATIBLE with MK VI MK VIIIEGPWS Honeywell HT 9000 KLN 89 KLN 90 HG2021AB GNS XEs IIMorrow Apollo 2101 Trimble 2100 2101 TNL8100 Universal GPS 950 UNS 1B Check manufacturer for compatibility with North South East West Velocities Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 64 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 5 5 RS 232 Transmit Receive 9600 baud Cat 3 ID 3 EGPWS MK VI MK VIII J2 RS 232 GPS peas s NE RX Receive In RS 232 M GPS Bus RX
47. CHANNEL CONN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE coer sss umm cgo mem BENI TANTUM TII E owu wopo pere ows PORE pe GPWS Warning Discrete 741 J1 78 DISC_OUT_1 Output Terrain Awareness Warning 747 2 Obstacle Awareness Warning 885 GPWS Alert Discrete 741 41 77 DISC_OUT_2 Output Terrain Awareness Caution 747 1 Obstacle Awareness Caution 41 76 DISC_OUT_3 Output Glideslope Cancel Discrete 7 4 6 41 73 DISC_OUT_4 Output Flap Override Discrete 7 4 5 J1 69 DISC_OUT_5 Output Audio On Discrete 7 4 2 J1 54 DISC_OUT_6 Output Terrain Display Select 1 Discrete 7 4 4 Terrain Awareness Caution or Warning E J1 51 DISC OUT 8 Output Obstacle Awareness Caution or Warning 7 4 7 3 Gnd Terrain Pop Up J1 49 DISC OUT 9 Output Terrain Display Select 2 Discrete 7 4 4 1 5 i unm J2 15 28V DISC 13 Not Defined in this ID Note 3 E 1 50 MON OUT 3 Output Not Defined in this ID Note 3 EL J1 52 DISC OUT 7 Output Not Defined in this ID Note 3 a x Possible States Type 1 Type 2 2 Flashing Lamps Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word
48. CUSTOMER WORKSHEETI A 137 APPENDIX B SAMPLE WIRING DIAGRAMS 141 APPENDIX C WINVIEWS OPERATION INSTRUCTION S 146 APPENDIX D VENDOR CONTACT INFORMATTION 150 APPENDIX E INTERFACE DESCRIPTION DOCUMENITLI 153 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 10 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION GENERAL INFORMATION Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 11 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION GENERAL INFORMATION SECTION GENERAL INFORMATION 13 T INTRODUGTION 2 ee ete 13 1 2 APPLICABILITY aan 13 1 3 HOW TOUSE THIS DOCUMENTS u nrbe w is 13 1A REFERENCE DOCUMENTS
49. GND Landing Flaps Discrete Landing Flaps gt Landing Flaps or Flap Override Not Landing Flaps gt Not Landing Flaps 6 6 5 28V Landing Flap Discrete Type Supplied by Flap or Flap selector handle switch Signal Status Landing Flaps or Not Landing Flaps Fault monitoring Indication of landing flaps selected for more than 60 seconds at airspeeds above 250 180 for GA Slow knots will result in a flap switch fault which will cause a GPW INOP indication Note This can be caused by either a flap switch fault or by the Flap Override switch being left in the on position Level 6 Audio readout 28 V Landing Flaps Discrete Landing Flaps gt Landing Flaps or Flap Override Not Landing Flaps gt Not Landing Flaps 6 6 6 Momentary Flap Override Discrete Type Supplied by a momentarily actuated cockpit switch Signal Status Flap Override activated if not active or Flap Override canceled if currently active Fault Monitoring Activation of this input continuously for more than 15 seconds will result in the Momentary Flap Override Invalid fault which will cause a GPW INOP indication Level 6 Audio readout Momentary Flap Override Flap Override Selected gt Flap Override Flap Override Not Selected gt Not Flap Override 6 6 7 Self Test Discrete Type Supplied by a momentarily actuated cockpit self test switch Signal Status Self Test or Normal Fault Monitoring Activation of t
50. Ground GND J1 53 OAT PROBE ELEMENT Note Nominal 500 Temperature Probe only Resistance 0 C 5000 0 60 Connection example CIC Temperature Sensor P N 05257 2 wire Connect positive lead to both J1 25 and J1 63 Connect negative lead to both J1 44 and J1 53 Chassis Ground Other probes may have three contacts Computed Airspeed Substitute Ground Speed for Airspeed airspeed is not available with this air data input CHANNEL PIN FUNCTION CONNECTION PIN TYPE DESIGNATION Polarity Configuration References REFERENCE Barometric Altitude J1 9 Input 28V DISC 08 gt 17V Valid 6 6 22 Validity Discrete 28V lt 4 4V Invalid 4 2 7 Derive Baro Altitude Rate Analog Baro Altitude Rate is derived using Uncorrected Barometric Altitude Although the ADC s provide Baro Rate the EGPWS does not have an analog connection available Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 184 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 12 AIR DATA INPUT SELECT 12 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format DC with Validity Flag Uncorrected Barometric J1 62 Input Type Basic Altitude gt 11 43 Fault Designation BAROMETRIC ALTITUDE FAULT Validity Barometric Alt Valid 28V kawa Airspeed No Substitute Ground Speed for Airspeed airspeed is not available with this air data CHANNEL
51. J1 59 72 Bee CEN EUN 453TX 2 B J1 57 72 Display Input Control Group 0 CHANNEL CONNECT KCPB IND Bus 1 out Fault Designation KCPB BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 CHANNEL CONNECT TO KCPB IND Bus 2 out Fault Designation KCPB BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 429TX 2 No Connection No Data Output Integration Notes 1 When interfacing to a single display controller configuration the Display Input bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 KCPB Keyed Component Picture Bus is also known as ASPB
52. MK VI MK VIII EGPWS CONFIGURATION MODULE SHEET 35 Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 4 Install item 1 3 Backshell Housing onto connector using item 1 8 Screws as shown in figure 2 1 4 below Ground Wire used for electrostatic discharge ESD protection is terminated with shielded pigtails of wires at this connector Q NM 2 t Ground Wire ESD 8690 990990 FIGURE 2 1 4 MK VI MK VIII EGPWS CONFIGURATION MODULE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 36 Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 5 Install item 1 6 Spring Clip as shown figure 2 1 5 below 8 ITEM 1 26 Spring Clip all e FIGURE 2 1 5 MK VI MK VIII EGPWS CONFIGURATION MODULE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 37 Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 6 Organize and dress wiring exiting from backshell Route Configuration Module wires exiting from connector then coil as shown in figure 2 1 6 below Install item 1 9 Cable Clamp as shown Do not tighten screws yet ITEM 1 9 Cable Clamp FIGURE 2 1 6 MK
53. MK VIII EGPWS Generic AFM Supplement MK VI MK VIII Enhanced GPWS Pilot s Guide MK VIII Bizjet Flight Test Procedure Flight Test Procedure for EGPWS with Internal GPS card MK VI MK VIII GA Fast GA Slow General Flight Test Procedure MK VI MK VIII Installation Ground Test Procedure Trouble Shooting Guide MK VI MK VIII Failures Modes Effects and Safety Analysis MK VI MK VIII Failure Modes Effects and Criticality Analysis Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 14 Honeywell MK VI MK VIII EGPWS Installation Design Guide 1 5 Description of Equipment The MK VI MK VIII EGPWS is a rack mount ground proximity warning GPWS and terrain awareness and warning Class A TAWS computer Some of the system features include Basic Ground Proximity Warning Modes 1 5 Mode 6 Altitude Callouts and Bank Angle alert Terrain Clearance Floor Terrain and Obstacle Awareness alert and display Terrain map with runways gt 2000 feet in length optionally gt 3500 feet in length on the MK VIII EGPWS Internal GPS card MK VI 965 1190 MK VIII 965 1220 0XX only Front loading updateable database requires Smart cable External Configuration Module with a Real Time Clock for use with Internal GPS Internal heater blanket for operation outside of the heated area of the aircraft Fixed Gear operation 1 5 1 MK VI EGP WS Computer
54. Reference Reasonable Range AIC FIFO LSB 0 00549316 Pitch Angle deg 1 deg deg Input Signal Connection 1 5 7 2 1 6 AIC Status Mask 0000010F External Validity Type Discrete Validity 6 1 13 Uncorrected Barometric Altitude CIC 02702 Signal Reasonable Range 1000 to 40 000 Feet 11 62 J1 43 D2 DC2 2 Feet Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 274 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 1 14 ARINC 547 578 4 Low Level Glideslope Deviation Validit Data Item Value Low Level Glideslope Validity DC Signal AIC Algorithm DC Absolute Signal Dynamic Range Signal Reasonable Range 0 5 to 1 5 VDC Signal Open Wire Threshold VDC Reference Dynamic Range Reference Reasonable Range S Validity VDC Input Signal Connection 1 30 10 Input Reference Connection External Validity Flag Connection 4 DC4 AIC Name DA DC4 2 0012207 VDC AIC LSB 00012207 VDC O AIC Status Mask 000200 External Validity Type lone 6 1 15 Roll Attitude 3 Wire Synchro 11 8 VAC with Validity AIC Algorithm 3 Wire Synchro 11 8 VAC Signal Name Roll Attitude 3 Wire Synchro Signal Dynamic Range 90 Synchro Angle 15 5 VAC max Data Item Signal Reasonable Range x80 Synchro
55. The MK VI EGPWS computer is available under P N 965 1180 without internal GPS and P N 965 1190 with internal GPS MK VI EGPWS computer is intended for small turboprop aircraft that provide a mixture of analog and digital interfaces The type of supported displays is limited and does not typically include EFIS displays Collins ProLine and Bendix EFIS 40 50 are supported The terrain database included with the MK VI EGPWS computer is regional having three separately defined databases for the AMERICAS North amp South America ATLANTIC Europe Asia Africa and PACIFIC Asia Australia 1 5 2 MK VIII EGP WS Computer The MK VIII EGPWS computer is available under P N 965 1210 without internal GPS and P N 965 1220 with internal GPS The MK VIII EGPWS computer is intended for regional turboprop and small turbofan aircraft that provide a mixture of analog and digital interfaces The type of supported displays is limited and includes some EFIS displays The terrain database included with the MK VIII EGPWS computer is global 1 5 3 MK VI MK VIII EGPWS Configuration Module The MK VI MK VIII EGPWS Configuration Module is available under P N 700 1710 020 The MK VI MK VIII EGPWS use a Configuration Module installed in the aircraft wiring to store aircraft EGPWS interface configuration and includes a Real Time Clock for EGPWS installations using internal GPS The Configuration Module is read by the EGPWS only during p
56. The output consist of internal parameters that can be used for display selection test purposes and discrete outputs that can be used for discrete outputs test and recording During LRU Self Test the SSM of each output label is set to the Functional Test status code The output types can be summarized as follows 1 Internal data Some internal data is output for test purposes only such as Radio Altitude Computed Airspeed Geometric Altitude etc 2 Alert status Each type of Voice and Lamp activity is mapped to a specific label BIT This can be used to provide inputs to display systems and flight recorders 3 Internal Mode status Various internal EGPWC mode logic is transmitted for test purposes 4 Terrain Display messages for TAD cockpit integration The ARINC 429 bus transmits both discrete and BNR labels In the event of catastrophic computer failure or 429 transmitter failure outputs will not be transmitted During Self Test the SSM will be set to functional test on all outputs bits 31 30 1 0 During all other conditions of computer or input failures the 429 outputs will continue to be transmitted as actual valid data For valid status the standard discrete SSM format is used 00 except for data indicated as being in 2 s complement format where the standard BNR SSM format is used 11 The SDI bits 9 10 will always be set to 00 Note Label 067 includes an indication of parameter inaccuracy that is not tied to the abo
57. y s Display bus type Honeywell picture bus DISPLAY BUS 1 2 CONNECT TO 453TX 1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 B J1 59 Display Input Control Group 248 CHANNEL CONNECT TO IC600 1 FDR Bus Fault Designation FDR BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Tvpe Basic 5 3 7 72 J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms J2 36 6 2 23 050 11 14 2000NM Basic N A 100 max Discrete Word 6 2 28 275 Bit 17 Discrete Basic N A 500 CHANNEL CONNECT TO 600 2 FDR Bus Fault Designation FDR BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range 6 2 23 050 Bits 11 14 2000NM Basic N A 100 max Discrete Word 6 2 28 275 Bit 17 Discrete Basic N A 500 Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed A J2 43 B J2 42 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x and 7 1 6 x 429TX 2 No Connection No Data Output Integration Notes The EGPWS ARINC 429 Output Bus must be connected to the display Display channels 1 and 2 are multiplexed on ARINC 453 Bus The Terrain display will Pop Up in response to EGPWS label 274 bit 28 Left display and bit 29 right display The system has only one range for terrain display on MF
58. 0 Fs me False C mee mee Rue 7 Ce 7 WGs E uz 89 True False Tre Tue Fase Fase 0 90 True False True Tre False Tre WGS84 020 96 Tre Tre False False WGS 84 020 98 True Tre False False False True WGS 84 020 99 Tre Tre Fase False Fase Tre 020 uma uut ume ee Hl MS D 112 Tre Tre True Fal False Falke WGS 84 020 3 Tme f Ime Pase f Fale 0 iis Te Fase Fase Tre 116 True True True False Tre False WGS 84 020 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 243 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 8 Category 8 Radio Altitude Input Select The following table provides identification of the Radio Altitude type The entry in the Radio Altitude Type corresponds to a table that provides detailed information on the configuration For example the details for Radio Altitude Type 1 are found in Table 5 3 8 1 ARINC 552 ALT 55 and digital ARINC 429 compatible Radio Altimeters are supported ALT50 Radio Altimeters are not recommended due to the maximum 2000 foot operation GPWS TSO C92c requires Mode 1 alert thresholds up to 2450 feet radio altitude In this category
59. 2 Ww er 310N 336 NI HOLIMS 123136 NIHOLIMS LISIHNI NIVH331L dONI NIVH33 L AV HH 19313S NIVHS3LL NI H3MOd OGA8Z NI H3MOd 100 dN dOd NIVYYIL 1nO 8 8807 100 8491 31ON 33S NI 8 62 SONVY AV dSIG 270 NI 8 62 SONVY AVTdSIG ON NI V 62 SONVY AVTdSIG ON NI V SONVY 14610 2 0 3431 ndNOO SNINHVM A LINIXO3d IIIWIA 5 62v NI YL SNE 1OHLNOO 62 ALON 33S asng esr Ano v sng HVOVMH H3HLV3M SNDI XIQN38 Proprietary notice on title page applies CAGE CODE SHEET 80 060 4314 150 REV DWG NO A NONE SIZE SCALE 97896 Honeywell MK VI MK VIII EGPWS Installation Design Guide 589 IWNYSLNIM SMd93 IIIA 020 022 696 SMd93 IIIA 020 0 21 996 Sd9 TIVNH31NI M SMd93 020 061 G96 SMd93 020 081 596 SH38IAQN LYYd SMd93 OL GALYOddNS LON SI NOLLVHOOIHNOO SIHL r NOILVYNSISNOOD 3883 JHL SI 2 1 3dAL 31330514 L AHOO931VO IHL NOILVYNSISNOD Q3SIQO33 JHL SI 08 0 5143 GALVYOSLNI 01 3dAL 14610 9 AHOO31VO IHL SYVOVY ONDI XION38 JHL OL 313 1dWOO L WANYW SIHL 30 NOLLO3S YSHLVAM JHL Ol 48334 7 8dO9 IHL ANY SNG V1VO 65 SHL HOS 318V2 Xvuavno
60. 2 321 General eat eee UR 29 2 3 2 MK VI MK VIII Computer Location nnne 29 2 3 3 MK MK VIII Computer Installation eee eee eene 30 2 3 4 Configuration Module Location esee eene eene nennen enetne trennen triente 31 2 3 5 Configuration Module Installation deter tee mt ei eee 31 2 3 6 GPS Antenna location s attese o etin edet en sR 40 2 3 7 GPS Antenna Installationz oen ted aeter dete deiade ate td eden 40 2 3 Sensor LOCA ON t u epe tle doe ua eese e ee totus euet eerte niae ene gru esae este nahe 40 2 3 9 OAT Sensor Installation ite de ide e e e e E E 40 2 310 Cockpit Lights s use etti een boe b ee ie bo etie be e eir b 40 2 3 10 1 D scriptiotiz sce e cerea ter dee De pee ded pid ree b de be da d e dee oett 41 VO CAM OM PEE 42 SECTION III SYSTEM 1 01 2 1 senatu sonata 51 BL INTRODUCTION 51 3 2 SYSTEM WIRING ELECTRICAL INTERFACES 22 51 3 2 T Primaty Power Input e e et e e Hei eer ad ol te cae 51 3 2 2 Chassis GIOUNG
61. 2 ARING 429 Input B leg SE Dev ange W2 RS l2 np eg Spare RS 232 Input Rev J2 11 lt 232 IN Spare RS 422 Input A leg SCI EEG UI Range 2 RS 422 Input B leg GPS RS 422 Input B leg LI S J2 26 429 OUT ms EGPWS ARINC 429 Output 2 A leg Proprietary notice on title page applies CAGE CODE 97896 SCALE SIZE A DWG NO 060 4314 150 REV SHEET 134 Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name GPWS 965 0686 001 020 Signal Type lt s Signal Name MK VI MK VIII EGPWS Enhanced Spare RS 232 Input Tx lt iid aba Spare RS 422 Input A leg J2 28 GPS Spare RS 232 Common lt 232 IN A GPS RS 232 Input Rev Spare RS 422 Input A leg 2 an Configuration Module Serial Input Display Range 1 ARINC 429 Input B leg J2 36 lt 429 input B SCI Display Range 1 RS 422 Input A leg IOC 1 ARINC 429 Input B leg Display Range 1 ARINC 429 Input A leg J2 37 lt 429 input A SCI Display Range 1 RS 422 Input B leg IOC 1 ARINC 429 Input A leg Air Data ARINC 429 Input leg P lt S A IOC 1 Nav ARINC 429 Input B leg Air Data ARINC 429 Input leg PE SAR AN IOC 1 Nav ARINC 429 Input A leg B A eet an ao oie EDITT EET M ree ERE c Sl UE UNE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 135 Honeywell
62. 9 ID 250 255 Navigation Input Select Type 250 255 IOC bus or equivalent are dual high speed digital ARINC 429 buses having the following labels 250 100 163 173 and 174 253 173 and 174 251 100 173 and 174 254 163 173 and 174 252 173 and 174 255 117 and 116 For interface description see paragraph 3 4 5 Air Data Type 255 Note ID 252 uses a special interface to input channels 2 and 5 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 96 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 11 8 Instructions Using Appendix E Tables 5 2 5 3 9 and 5 3 9 x as described above select the Navigation Input Select Type that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Navigation Inputs Select Type from Appendix E Table 5 3 9 under the Ident No heading for Step Category 9 in Appendix E Table 5 2 Using the Navigation Inputs Select number from Appendix E Table 5 3 9 as x go to Appendix E Table 5 3 9 x The electrical interfaces pin outs for the Navigation Inputs Select Type are shown in Appendix E Table 5 3 9 x and are used to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 97 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 12 Category 1
63. Alternate Mode Awareness Enable Reversal Reference Effectivity Enabled Pop Up Enabled 2 Enabled L36 f Fae f Fale WGS 84 ras ce False False Tus 39 False True False True Tue Mst 020 True 60 False True Tre True Tre Fase WGS 84 020 61 Fase True Tre Tue Tre Fase ML 020 False Ime Ime f Ine Tue wassa _ 7 66 Tre Fase Fase False Fase Tue WGS 4 420 68 True False False False Tre Fase WGS 84 020 69 True False False False True Fase 020 4 True Kase Tue wosst 00 75 True False False Tre False True 020 76 Tre False Fase Tre WGS 84 00 TS E 80 True False True False False WGS 84 020 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 242 Honeywell MK VI MK VIII EGPWS Installation Design Guide Steep TA amp D Peaks Obstacle Bank Angle Flap GPS Altitude Software Approach Alternate Mode Awareness Enable Reversal Reference Effectivity Enabled Pop Up Enabled 2 Enabled Tme _ _False_ _True_ _False_ _ Trme Tue wasse
64. At the time of release of this document all GPS sources except the Universal GPS1000 based systems are of MSL type The Universal GPS1000 based GPS sources are of WGS 84 type If the internal GPS source ID 2 is defined the GPS altitude reference in Category 7 must be MSL NOTE 2 ID 10 11 12 13 and 253 may only be used when pitch and roll attitude inputs are configured for use in Category 10 Attitude Input Select Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 187 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 3 0 Position Input Type 0 Low Speed ARINC 743A GPS CHANNEL CONNECT TO GPS ARINC 743A Fault Designation GPS BUS 429 4 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 000 Longitude Normal 6 2 8 20 180 Degrees Basic 0 00017166137695 000 GPS Hor Int Limit 6 2 5 7 16 nm Basic 0 00012207 000 Altitude 6 2 4 20 131 072 FT Basic 0 125 000 VFOM 6 2 13 oo 32768 ft Basic 0 125 000 16 0 000061035 000 4096 Knots Basic 0 125 000 180 Degrees Basic 0 005493 1640625 000 24096 Knots Basic 0 125 000 4096 Knots Basic 0 125 000 32768 fpm Basic 1 000 Discrete Wd Basic n a 000 Discrete Wd Basic 0 1 min 000 Discrete Wd Basic 1 day 000 HFOM 6 2 10 Ground Speed 6 2 6 True Track Angle 6
65. Data Glideslope Localizer Reference Fault Designation IOC BUS 1 Bus Type Basic Label Sig Bits Range 6 2 30 6 2 33 174 173 5 0 8 DDM 0 4 DDM Signal Type Resolution Rate ms Basic Basic 0 0001953125 0 00009765625 33 3 66 6 33 3 66 6 CHANNEL CONNECT TO IOC 2 Fault IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Type Basic A J2 21 J2 04 P P 1 J2 37 2 36 CHANNEL CONNECT TO IOC 2 429RX 3 Format ARINC 429 High Speed A J2 41 B J2 40 CHANNEL 429 422RX 1 CHANNEL CONNECT TO IOC 2 429RX 3 Format ARINC 429 High Speed 1 A J2 37 B J2 36 CHANNEL CONNECT TO IOC 2 429RX 3 Format ARINC 429 High Speed A J2 41 B J2 40 Data Glideslope Localizer Reference Label Sig Bits Range 6 2 30 6 2 33 174 173 8 DDM 4 DDM Signal Type Resolution Rate ms Basic Basic Table 5 3 9 253 Navigation Inputs Select 253 CONNECT TO IOC 1 Format ARINC 429 High Speed Data Glideslope Localizer Data Glideslope Localizer Reference Fault Designation IOC BUS 1 Bus T Label pe Basic Sig Bits Range Signal Type 0 0001953125 0 00009765625 Resolution 33 3 66 6 33 3 66 6 Rate ms 6 2 30 6 2 33 Reference 174 173 Fault Designation IOC BUS 2 Bus T Label 12 12 pe Basic Sig Bits 50 8 DDM 0 4 DDM
66. MK VI MK VIII EGPWS Installation Design Guide Signal Name GPWS 965 0686 001 020 Signal Type 4 m Signal Name MK VI MK VIII EGPWS Enhanced Ground pS ANT GPS COAX Connection Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 136 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX A Customer Worksheet Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 137 Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 138 MK VI MK VIII EGPWS Honeywell CUSTOMER INTERFACE WORK SHEET DATE The purpose for this work sheet is to obtain the necessary aircraft data for determining the specific interface configuration for the MK VI or MK VIII Enhanced Ground Proximity Warning System EGPWS For defined MK VI and MK VIII EGPWS interface data refer to Appendix E nterface Description Document IDD for the Mark VI and VIII Enhanced Ground Proximity Warning System MKVI VIII EGPWS For product description information refer to Honeywell document No 965 1176 601 Product Specification for the Mark VI and VIII Enhanced Ground Proximity Warning System Contact Honeywell EGPWS Applications Engineering for assistance 800 813 2099 or 425 885 871
67. MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 240 Collins Pro Line 21 Integrated with overlay Peaks Elevations MK VIII Only Display Configuration Group 245 Function Reference section Display Type Collins ProLine 21 Integrated with overlay peaks elevations and partial compass raster patch Sweep Type Fan Mode with 90 degree limit Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Category 7 does not affect pop up logic The display controls pop up therefore enable disable of pop up is done via the display Peaks Mode 5 3 Peaks Enable True Peaks On Manual Deselect Deselection is controlled by display Yes 10 NM controlled by display Moving Marker 14 Overlay Page Yes for Peaks Elevations only located upper right side of display Y l O O Display bus type ARINC Compatible Format Collins ProLine 21 label 077 Terrain Mode ProLine 21 system outputs Terrain Mode annunciation it does not use Annunciation EGPWS ASCII message DISPLAY BUS 1 CONNECT TO SE OT A J1 58 Terrain Display data to Primary Flight Display Multi Function display 1 ca DISPLAY BUS 2 CONNECT TO i ee B 1 57 Display Input Control Group 254 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429RX_1 Format ARINC 429 High Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range
68. Qu edite ite der h u q Mi aa a u 20 18 3 Flight History Card us a a no Gata Su eet ie edge dtes ue aa qhaya uha 20 1 9 ACCESSORIES NOT SUPPEIED horrere D metet rete PIE Ie aoro uae to Irt pot 20 1 9 1 ARINC 453 Terrain Display wiring 20 1 9 2 GPS Antenna Cable P ERI qs 21 1 03 Circuit BEOOkOE reet et eot k 21 1 9 4 Annunciators amp Switch Annunciators n eese eee eee hne 22 7 03 Cockpit Speakers s 23 1 9 6 d A os ede pede repe eode ett G ee Mite dl 23 PLO TOOLS REQUIRED eerte tro a uta P NER aaa EUER SERERE EN Ee qupa Sa 24 LAO Crimping Tool PT P2 P3 ted dede t t dde tn DA he 24 410 2 Contact Positioner PE P2 P3 Lee niet a ua 24 1 10 3 Insertion Removal Tool P1 202 24 1 10 4 Spare Connectors and Contacts P1 P2 25 ISELEICENSE REQUIREMENTS 5 I reete oe E e I RET RE He a PET EIER EQ e FIOR q IRE 25 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 12 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION GENERAL INFORMATION 1 1 Int
69. RawCAS1 MFIpOvrd RawBaroRt1 LandGrDsc AUBaroVal HiLandGrDsc RawAACSAT GndLandGrDs RawSAT1 GSCan ILSTuned1 TerrDis AGS1Val AudInhDsc RawAACGS1 GPWSInhDsc ALoc1Val M6LwVolDsc RawAACLoc1 APEngDisc1 RawGS1 GSInh RawLoc1 StpAppSel RawGLat1 MomSASel GPSLatude1 TAWxRng1 RawGLng1 TAWXxRng2 GPSLngude1 DispRngOut1 RawGAIt1 DispRngOut2 RawHFOM 1 PosUncert RawVFOM1 GPWInop RawRoll1 WSInop RawPitch1 TA NotAvail Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 148 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX D VENDOR CONTACT INFORMATION CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 149 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX D Vendor Contact Information Vendor Contact Information The vendor contact information provided below is current at the time of publication of this document AMP Amphenol Avidyne Corporation Avtech Corporation Barry Controls BF Goodrich Aerospace Computer Instruments Corp Comant Dallas Avionics Inc Eaton Corporation see Dallas Avionics EDMO Distributors Inc CAGE CODE 97896 SCALE NONE SIZE A 2800 Fulling Mill Road MS 038 035 Middletown PA 17507 800 806 0480 20 Melford Drive Scarborough Ontario Canada M1B 2X6 Ph 416 291 4401 Fax 416 292 0647 55 Old Bedford Road Lincoln MA 01773 Ph 888 723 7592 3400 Wal
70. Spr 0 0 0 0 24 2 14 Spr 0 0 0 0 00 BE 15 Spr 4 17 Character Code LeftMostofSetlof6 16 6 O 18 Character Code LeftMostofSetlof6_ 7 7 7 37 7 7 19 Character Code LeftMostofSetlof6 Bs 38 8 O 20 Character Code LeftMostofSetlof6 9 9 9 Character Code Left Most ______________ 2 23 Character Code Lefi Most of Set of6 NSB bR He 2 Character Code Next Most of Set2of6 LSB 7bitHex 2C 3C lt 4 Charter Cade Next Mest of E o e O 25 Character Code Next Most of Set 2of6 2 385 gt 26 Character Code NextMostofSet2of6 3F 27 Code Next Most of Set of Continued at 28 Character Code NextMostofSet2of6 LABEL 054 Below 29 Character Code Next Most of Set2of6 MSB 7bitHex Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 311 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 3 5 Message Word 3 054 This label contains the second 2 characters to be displayed on the 6 character terrain display window 910 sproo Spare Contimed from 12 Spare 0 13 Spare J s o P 4 Sm SSS os Degg Li 0 15
71. The MK VI EGPWS only supports aircraft types 0 1 2 3 4 that are designed for turboprop aircraft and emulate the mode curves of the MK VI GPWS The MK VIII EGPWS has Aircraft types 254 amp 255 that are designed for turbofan aircraft and emulate the mode curves of the MK V GPWS along with aircraft types 0 1 2 3 4 Modes 1 2 3 amp 4 are different between these aircraft types For reference compare the mode 1 4 turbofan curves to the turboprop curves in the MK VI VIII EGPWS Product Specification 965 1180 601 Appendix E Table 5 3 1 lists the combinations of Aircraft Mode Types identifies the first MK VI MK VIII EGPWS version in which the option was available see the Effectivity entry and describes the options available with each Aircraft Mode type see Description column 3 3 2 Mode 1 type Two Mode 1 alert curves are defined GA Turboprop and Bizjet Turbofan The lower boundary of the GA Mode 1 curves is 50 feet the same lower boundary is extended to 10 feet for Bizjet aircraft 3 3 3 Mode 2 type Two Mode 2 alert curves are defined one for GA Fast amp Bizjet and one for GA Slow Mode airspeed expansion increases the Mode 2 expanded alert area linearly from 1650 feet to 2450 feet for airspeeds of 220 knots to 310 knots in GA Fast and Bizjet defined aircraft same as MK V and MK VII EGPWS Mode 2 airspeed expansion occurs for airspeeds from 190 knots to 280 knots in GA Slow defined aircraft MODE 2 AIRSPE
72. 0000 9000 720 SHIM Q3Q 13IHS Z000 9Z1 ZLW ASN L S31ON NI 313889SIQ 03193135 NiVHH31 ZZ S9rd NI 31359514 NiVHH31 7 al 99rd NI Y Sn8 69 22 q gas 862v H3llINSNVHIl H 18 a LNO V H3lllNSNVHII H 89 az 59 9S ONIM XIGNAG 1O8WAS a a AV LN3INOW sna YOLYIONNNNY 1S31 OL SS3Hd MOLVIONNINNY NO 385 NOILOW 1 11 SMd93 AISIHNI NIVHH3L lt e gt o SOINOIAV 20 82 10 336 SION 336 1531 01 553 YOLVIONNNNG 2508 YOLVIONNNNY SMd93 LON 336 LON 385 e 45 ov 09 65 85 0 96 Ww er NI HOLIMS 1237135 NI HOLIMS LISIHNI NIVH3I3 L dONI 100 19313S NIVHH3 L NI 43MOd NI 43MOd OGASZ 100 dfrdOd NIVYY3L 100 8 8491 INO V 8829 ILON 335 NI 8 627 AV dSIG 2 ON NI 8 SONVY AV dSIG ON NI V SONVY AV dSIG ON NI V SONVY AV dSIG Z ON M3lndWOO SNINHVM ALIWIXONd ANNOYS Q39NVHN3 IIIWIA MeV 100 8 sng viva esr 100 v sna v1va esr ALON 385 NI 8 Sn8 1OM1NOO 62 NI VI SNE 1OH1NOO 627 H3HIV3M SNDI XION38 Proprietary notice
73. 1 1 O C anner n Connector FIGURE 2 1 1 MK VI MK VIII EGPWS CONFIGURATION MODULE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 33 Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 2 Wire item 2 0 Configuration Module This part will replace item 1 4 Backshell plate Install the pre crimped colored wires into item 1 1 Connector as shown in figure 2 1 2 below VIO C17 BLU 16 NA ORN 55 md BLK 50 D 6 WHT m 49 6 9 m 592 RED 32 920 996 Connect 020 O20 O96 929 2 0 Configuration O26 859 Module Ground Wire Will be terminated REAR VIEW at Step 4 FIGURE 2 1 2 MK VI MK VIII EGPWS CONFIGURATION MODULE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 34 Position item 1 7 Slide lock onto wired connector as shown in figure 2 1 3 below 9990 amp 06 e wW 5 M N 9999 69669606600 al REAR VIEW FIGURE 2 1 3 Honeywell MK VI MK VIII EGPWS Installation Design Guide Connector inc Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A 53 DWG 060 4314 150 REV ide Lock
74. 10 Attitude Type 0 Category 11 Heading Type 0 Category 12 Windshear select Type 0 Category 13 Discrete I O Type 0 Category 14 Audio Output Level Type 0 Category 15 Undefined Type 0 CMR list based on the previous configuration CFG gt CMR lt Enter gt CONFIGURATION MODULE Format Version Category 1 ID Category 2 ID Category 3 ID Category 4 ID Category 5 ID Category 6 ID Category 7 ID Category 8 ID Category 9 ID Category 10 ID Category 11 ID Category 12 ID Category 13 ID Category 14 ID Category 15 ID CRC 527518533 e or Oe Proprietary notice title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 121 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 5 2 Configuration Module Reprogramming Reprogramming the EGPWS Configuration Module is accomplished similar to the programming process above Prior to reprogramming the desired new configuration should be determined based on the MK VI VIII Interface Description Document Appendix E document number 060 4314 401 For reprogramming the Configuration Module the following procedure is used 1 Verify EGPWC interface to P2 connector including Configuration Module and RS 232 interface to PC 2 Power EGPWC and PC and start WinVIEWS 3 With WinVIEWS active in the Terminal Mode start the Configuration sub mode by typing CFG at the prompt gt At this point either all the ID s c
75. 11 180 degrees Basic 0 087890625 200 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Glideslope 6 2 30 12 0 8 DDM Basic 0 0001953125 33 3 66 6 Localizer 6 2 33 12 0 4 DDM Basic 0 00009765625 33 3 66 6 PFD Mode Select Word 6 2 44 Discrete Type 4 Basic n a 250 Selected Course 6 2 61 11 180 degrees Basic 0 087890625 200 Glideslope Deviation Localizer Deviation CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Basic Data Reference Range Signal Type Resolution Rate ms Glideslope 6 2 30 0 8 DDM Basic 0 0001953125 33 3 100 Localizer 6 2 33 0 4 DDM Basic 0 00009765625 33 3 100 Selected Course 6 2 61 180 degrees Basic 0 087890625 33 3 100 Data Reference Range Signal Type Resolution Rate ms Glideslope 6 2 30 0 8 DDM Basic 0 0001953125 33 3 100 Localizer 6 2 33 0 4 DDM Basic 0 00009765625 33 3 100 Selected Course 6 2 61 180 degrees Basic 0 087890625 33 3 100 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 250 422RX_1 A J2 39 B J2 38 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 9 252 Navigation Inputs Select 252 CONNECT TO IOC 1 Format ARINC 429 High Speed
76. 150 REV SHEET 49 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 14 2 Dual ARINC 429 BUS Cat 14 ID 253 254 255 sese nnne nnne nnne 102 p 102 3 15 CATEGORY 13 INPUT OUTPUT DISCRETE TYPE 8 2424 000 00000000 AO TA 103 DASA InputDiscretes Eee to n E reed 103 3 15 1 1 Glideslope Inhibit Discrete cue iet itte tette ence in eoa e ena 103 3 15 1 2 Eandmeg Flaps Discrete a n deest dede ree E deer bleak eb E de rb EUR Ie EE ERES 103 3 15 1 3 Audio inhibit Discrete o cer D Ae ed ede n duet tec RH 3 15 1 4 Landing Gear Discrete 3 15 1 5 Glideslope Cancel Discrete 3 15 1 6 Momentary Flap Override Discrete soiirci o aE r E EE EEE EEE i EEEE Ea A iS 106 315 17 6 Low Volume Discretes a eb oe Ete d ee pe tied Adi dee e nbi 106 3 15 1 8 Autopilot Engaged Discrete irais Ona T EKE 107 3 15 1 9 Terrain Awareness and Inhibit 0 4111 00000000000 107 SAAS AAO Self Pest Discrete p Ghai bite iad a a Gaui bie IO HD CIUS 107 11 Steep Approach Discrete 32 redet E e EH A E EE E EEE ua REAA 108 3 15 1 12 GPWS INHIBIT Discrete alternate 108 3
77. 2 Internal GPS CHANNEL Internal GPS Fault Designation INTERNAL GPS Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude 6 4 1 32 E180 Degrees Basic single precision 1000 Longitude 6 4 1 32 180 Degrees Basic single precision 1000 HP Error 6 4 1 32 meters Basic single precision 1000 Altitude 6 4 2 meters Basic single precision 1000 VP Error 6 4 2 meters Basic single precision 1000 Ground Speed 6 4 3 meters sec Basic single precision 1000 True Track Angle 6 4 3 360 Degrees Basic single precision 1000 East Velocity 6 4 4 meters sec Basic single precision 1000 North Velocity 6 4 4 meters sec Basic single precision 1000 Vertical Velocity 6 4 4 meters sec Basic single precision 1000 GPS State 6 4 5 Discrete Wd Basic n a 1000 Integrity State 6 4 5 Discrete Wd Basic n a 1000 Error Status 6 4 5 Discrete Wd Basic n a 1000 Notes Slowest acceptable update rate in milliseconds 1l MSL reference must be selected when an internal GPS is utilized Refer to Table 5 3 7 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 188 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 3 3 Position Input Type 3 RS232 GPS PXpress format CHANNEL CONNECT TO GPS PXpress format Fault Designation GPS BUS Format RS232 9600 baud Bus Type Basic GPS_RXA 5 Data Reference Sig Bits Range Signal Type Res
78. 2 57 6 2 58 6 2 59 6 2 60 6 2 61 6 2 62 Honeywell MK VI MK VIII EGPWS Installation Design Guide Horizontal Figure Of Merit 247 GPS ARINC 7434 Horizontal Figure Of Merit 247 GPS ARINC 743 Horizontal Figure Of Merit from HDOP 101 GPS ARINC 743 Vertical Figure Of Merit 136 GPS ARINC 743A Vertical Figure Of Merit 136 GPS ARINC 743 Vertical Figure Of Merit from VDOP 102 GPS ARINC 743 Sensor Status 273 GPS Universal Time Correlation 125 GPS Date 260 GPS Control Word 154 MFD Control Word 2 271 273 Control Word 2 271 273 Type 2 Discrete Word 155 or 176 MFD Hazard Range Output 077 Range 050 Multifunction Signal Generator MG or IC600 Query Continuous Response 011 KCPB Key Press Data 012 KCPB Control Word 1 270 Discrete Word 273 Bendix Weather Radar Vertical Profile Mode Discrete Word 275 IC600 only Radio Altitude 164 Glideslope Deviation 174 or 117 Roll Angle 325 Magnetic Heading 320 Localizer Deviation 173 or 116 Pitch Angle 324 Range 271 KCPB DSU Status Word 350 True Heading 314 Corrected Barometric Altitude 204 Computed Airspeed 206 True Airspeed 210 Decision Height 370 IOC Scaling Normal Acceleration 333 Longitudinal Acceleration 331 Left Body Angle of Attack 224 Right Body Angle of Attack 225 VOR ILS Frequency 034 PFD Mode Select Word 163 FWC amp GP Discrete Word 171 Body Pitch Rate
79. 2 9 180 Degrees Basic 0 0054931640625 1000 North South Velocity 6 2 53 4096 Knots Basic 0 125 1000 East West Velocity 6 2 54 4096 Knots Basic 0 125 1000 Vertical Velocity 6 2 58 32768 fpm Basic 1 1000 Sensor Status 6 2 16 Discrete Wd Basic n a 1000 UTC 6 2 17 Discrete Wd Basic 0 1 min 1000 Date 6 2 18 Discrete Wd Basic 1 day 1000 NO NO Un tn tn tA CA OO Notes Slowest acceptable update rate in milliseconds This label is not required Data used if present Table 5 3 3 5 Position Input Type 5 High Speed ARINC 743 GPS CHANNEL CONNECT TO GPS ARINC 743 Fault Designation GPS BUS 429RX 4 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 20 180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 7 16 Basic 0 00012207 1000 Altitude 6 2 4 20 131 072 FT Basic 0 125 1000 VDOP 6 2 15 1024 Basic 0 03125 1000 HDOP 6 2 12 1024 Basic 0 03125 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125 1000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 1000 North South Velocity 6 2 53 4096 Knots Basic 1000 East West Velocity 6 2 54 4096 Knots Basic 1000 Vertical Velocity 6 2 58 32768 fpm Basic 1000 Sensor Status 6 2 16 Discrete Wd Basic 1000 UTC 6 2 17 Discrete Wd Basic 1 mi 1000 Date 6 2 18 Discrete Wd Basic 1000 Un
80. 28V lt 4 4 Invalid 4 2 7 DH Discrete Gnd J1 33 Input GND DISC 1 Gnd Below DH 6 6 14 not Gnd Above DH 42 7 Table 5 3 8 4 Radio Altitude Input Select Type 4 KRA 405 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format Alt 55 with Validity Flag KRA 405 Auxiliary Output 1 Radio Altimeter 1 11 64 Input Type Basic J1 45 Fault Designation RADIO ALTIMETER FAULT Validity Radio Altitude Valid Discrete 1 28V PIN FUNCTION CONNECTION PIN TYPE CHANNEL DESIGNATION Polarity Configuration References REFERENCE Radio Altitude Validity 28V_DISC_07 gt 17V Valid Discrete 1 28V lt 4 4 Invalid DH Discrete Gnd J1 33 Input GND_DISC_11 Gnd Below DH 6 6 14 lt not gt Gnd Above DH 4 2 7 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 245 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 8 251 Radio Altitude Input Select Type 251 ARINC 429 via dual IOC buses with DH MDA a CONNECT TO IOC 1 Fault Designation IOC BUS 1 a 1 Format ARINC 429 High Speed Bus Type Basic Data Reference Label xe Bc Range Signal Type Resolution Rate ms J2 37 Radio Altitude 6 2 29 164 8192 Basic 0 3 25 50 B J2 36 Decision Height MDA 6 2 62 170 12 14 4096 16384 1000 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Type Basic
81. 326 Body Roll Rate 327 Minimum Descent Altitude 170 IOC Scaling Normal Angle of Attack 236 North South Velocity 166 GPS East West Velocity 174 GPS Discrete Word 017 KMD 550 850 Inertial Vertical Speed 365 Inertial Altitude 361 Vertical Velocity 165 GPS Latitude Fine 120 GPS Longitude Fine 121 GPS Selected Course 100 IOC DH MDA Selected 170 DAU Scaling 6 3 DIGITAL DATA ARINC 575 6 3 1 6 3 2 Static Air Temperature 213 Uncorrected Barometric Altitude 203 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV 279 279 279 279 279 279 280 280 280 281 281 281 282 282 283 283 284 284 285 285 285 285 286 286 286 286 286 286 287 287 287 287 287 287 288 288 288 288 288 289 290 290 290 290 291 291 291 291 291 291 292 292 292 292 292 292 293 SHEET 156 6 3 3 6 3 4 Honeywell MK VI MK VIII EGPWS Installation Design Guide Barometric Altitude Rate 212 Computed Airspeed 206 64 DIGITAL DATA RS 232 6 4 1 6 4 2 6 4 3 6 4 4 6 4 5 Xpress GPS Packets ID 15 Lat Lon Estimated Horizontal Position Error Xpress GPS Packets ID 16 Altitude Estimated Vertical Position Error Xpress GPS Packets ID 17 Ground Speed Track Angle Xpress GPS Packets ID 18 East North Up Velocity Xpress GPS Packets ID GPS State 6 5 DIGITAL DATA RS 422 6 5 1 6 5 1 1 6 5 1 2 6 5 2
82. 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 36 Range 6 2 20 273 N A 5 320NM Basic N A 100 CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range 6 2 20 273 N A 5 320NM Basic N A 100 Output 429 Bus Group 1 Channel Comments 429TX_1 Low Speed 12 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x 2 42 Manual Deselect Deselection is controlled by display YV U O O 429 2 Low Speed A J2 26 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x B J2 9 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 FPI 9xx when not selected will command the display range to 10 NM and Pop Up to Terrain mode if there is a Terrain alert The range does not change if Terrain Mode is already selected when there is a Terrain Alert 3 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 222 Honeywell
83. 39 J3 25 Sperry VG 14A GG FF Q R Sperry VG 311 P1 45 1 8 1 9 Note 1 connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation Note 2 See LCR installation manual Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 98 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 12 3 Digital Pitch amp Roll Angle ARINC 429 High Speed Cat 10 ID 5 amp 6 EGPWS MK VI MK VIII _J2 AHRS 429 Bus oN ARINC 429 AHRS lt 23 XI ARINC 429 6 C crt P B High Speed Digital AHRS vsd Vendor Model Cat 10 ARINC 429 Bus 1 ARINC 429 Bus 2 ID A B A B Collins AHC 85 D E only 6 P1 16 P1 14 P1 24 P1 22 Litef LTR 81 AHRS 6 MP G7 MP G8 MP E5 6 Litef LCR 92 LCR 93 AHRS 6 J4 08 J4 29 J4 49 J4 07 Honeywell HG1075 1095 IRU 6 J1B G7 J1B G8 J1B E5 J1B E6 NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation ID 6 is preferred with Category 2 Air Data with ARINC 429 Barometric Altitude Rate label 212 otherwise ID 5 ID 6 cannot be used with analog Air Data interfaces 3 12 4 Digital ARINC 429 Dual
84. 4 2 Digital ARINC 429 Cat 2 ID 5 1 6 I3 eene enne nnn 3 4 3 Digital ARING 2725 Cat 2 ID 25 ciae er e e neat rod niae ere tede ad n n ei NI 3 4 4 Shadin 2000 Cat 2 ID 1022 8 eene eene nennen trennen entree terere nennen tenete nennen eren 3 4 5 Digital ARINC 429 Dual IOC Buses Cat 2 ID 255 ener nennen enne au CATEGORY 3 POSITION NPUT SEEBCT tete E QS 743 FOrm tu dade qute tb dedidit 3 5 2 GPS Altitude Label 076 Reference 3 5 3 North South East West Velocity labels 3 54 ARING 429 BUS Cat 14 5 10513 i epe te RERO RE EERE 3 5 5 RS 232 Transmit Receive 9600 baud Cat 3 ID 3 eene nete rennen 3 5 6 Dual ARINC 429 BUS Cat 3 ID 253 amp 255 isset enne eren ener enne 3 9 V AnSIFUCIOBS Ar 3 6 ALTITUDE C netto ee er ud erede e eo A 3 7 CATEGORY 5 AUDIO MENU SELECT E au e RD IEEE ORI OT RE 3 7 Audio Menu Selection snusar ninnan a i eee RR 3
85. 66 6 Localizer 6 2 33 Basic 0 00009765625 33 3 66 6 ILS Select VOR ILS Freq 6 2 46 Basic Bit 14 ILS 167 333 Configuration Data Reference Section KN40 Nav Source Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 249 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 9 5 Navigation Inputs Select 5 CONNECTION SUMMARY DATA Format ARINC 547 with Validity Flag amp ILS Select 1 65 Input Basic J1 46 Fault Designation GLIDESLOPE FAULT Validity Glideslope Validity Discrete 71 28V Format ARINC 547 with Validity Flag amp ILS Select 11 30 Input Type Basic J1 10 Fault Designation LOCALIZER FAULT Validity Glideslope Validity Discrete 1 28V REFERENCE Discrete 1 lt 4 4V Not Valid 42 7 Discrete 1 lt 4 4V Not Valid 42 7 Discrete 1 lt 4 4V ILS Not Tuned 42 7 GND ILS Tuned J1 20 Input GND DISC 01 Gnd ILS Tuned 6 6 8 Discrete 1 not Gnd ILS Not Tuned 4 2 7 Table 5 3 9 250 Navigation Inputs Select 250 CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Glideslope 6 2 30 12 0 8 DDM Basic 0 0001953125 33 3 66 6 Localizer 6 2 33 12 0 4 DDM Basic 0 00009765625 33 3 66 6 PFD Mode Select Word 6 2 44 Discrete Type4 Basic n a 250 Selected Course 6 2 61
86. 7 Output NotDefinedinthisID Note3 od Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word bit if configured by the display type Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 261 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 3 Input Output Discrete Type 3 DESIGNATION REFERENCE comer umm cgo mem EECINICT CANCTNI Int ose hse eg ad o Steep Approach Discrete 2 Note 2 Gnd Selected 32 31 alternate action lt not gt Gnd Not Selected J1 72 MON OUT 1 Output GPWS INOP Discrete i743 TAD INOP Discrete GPWS Warning Discrete 144 J1 78 DISC OUT 1 Output Terrain Awareness Warning 747 2 Obstacle Awareness Warning DN GPWS Alert Discrete 741 J1 77 DISC_OUT_2 Output Terrain Awareness Caution 747 1 Obstacle Awareness Caution 1 76 DISC OUT 3 Output Glideslope Cancel Discrete 746 ss J1 73 DISC_OUT_4 Output Flap Override Discrete 745 5959552 J1 69 DISC OUT 5 Output Audio On Discrete 742 ouput Terain Displey Deces Terain Select 2Dscete
87. 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 The EFIS BUS fault will be present only if both MG inputs have failed 3 Honeywell EFIS SG amp MG provide Terrain display relay control 4 display uses the following ARINC 429 labels from the EGPWS for annunciations The Terrain display will annunciate TERR in green or cyan depending on the program when the Terrain is selected and valid TERR in amber if Terrain is selected and any of the following conditions are TRUE e The EGPWS ARINC 429 output bus is missing or labels 050 and 051 or are absent or unreadable for 2 seconds EGPWS ARINC label 051 bit 13 0 Terrain Display Valid bit FALSE EGPWS ARINC label 050 bit 17 1 Terrain Inhibit bit TRUE EGPWS ARINC labels are valid but the range in label 050 disagrees with the range via SCI bus label 80 label 050 bit 11 14 contain left display bus range and bits 15 18 are the right display bus range Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 236 Honeywell MK VI MK VIII EGPWS Installation Design Guide The display will be blanked when the amber TERR is present The display will Pop Up to Terrain mode as follows If all the conditions indicated for the amber TERR above are FALSE If the display is in normal MFD mode
88. 8 CATEGORY 6 TERRAIN DISPLAY SELECT 3 0 d TADE A TCESelecfiQH i Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 48 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 8 2 Terrain Display Configuration Group cccccccceccscsssecssessceseescesesseesecseeecaseesesesseesecsecseesecsesseceeesceseeaeeaeseeeeneeeeenaes 70 26 22 Display Input Control Group iu dte t au yas die eg etel ore ete dio es e Breite eid eee ted 70 3 8 4 Output429 Bus Groups a l A L tacere eie n repe esee 71 310 3 IBSIFUCH OBSTa e eee FS ERREUR 71 3 6 6 Sample Display uy nil opp deii 71 3 9 CATEGORY 7 OPTIONS SELECT GROUP 1 1 4 01 enne nennen nennen enne 88 3 9 T Steep Approach iot mn dod ut a ase e els 88 3 9 2 TA amp D Alternate Pop Ups i edet e o D e ep our Eod Ae eot ee Ede 88 3 93 Peaks Mode ee el e ettet N i 88 3 94 Obstacle Awareness ix temen 88 3 9 5 Bank Angle Callout Enabling a hasa tiM tet aaa
89. ARINC 429 transmitter by means of a single twisted and shielded pair of wires The shield shall be grounded at both ends and at all production breaks in the cable to an aircraft ground close to the rack connector Receiver Bus Frequency Receivers are capable of operating at both Low and High speed and are determined by configuration selection The following table identifies the bus speed characteristics Bus Speed Bus Frequency High 100 KBPS 1 Low 12 0 KBPS to 14 5 KBPS ARINC Receiver Bus Identification Each ARINC Receiver Channel is identified with two identifiers one for each leg of the twisted wire pair The identifier is formed as follows 429RX Channel Id Leg where Channel Id ranges 1 8 and Leg is A for the positive leg and B for the negative leg see channel exception in following paragraph An example of a channel identifier would be 429RX 2A which identifies leg A of ARINC 429 channel 2 In addition one of the ARINC 429 channels is connected to an UART to provision for RS422 operation In this case the channel identifier has been defined as 429 422 1A and 429 422RX 1B SIGN STATUS Matrix The number of BITS and the meaning of these BITS varies depending on the type of data in the ARINC word Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 276 Honeywell MK VI MK VIII EGPWS Installation Design Guide BINARY BNR DATA BIT31 BIT30 DEFI
90. AlliedSignal Picture Bus 3 Label 012 is optional The current fault and fault history message RANGE for label 271 Range is not shown if Range Keys are requested on label 012 Key Press Display Mode 4 The Display group is configured by the Display using response labels on its ARINC 429 data bus 5 KCPB bus types use Inop amp Warning Annunciations in same Window therefore during EGPWS Self Test the Fail lights will not remain on throughout the test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 215 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 19 KC Picture Bus with Soft Keys Display Configuration Group 0 Display Type KC PictureBus KCPBY 2 Sweep Type Curtain Vertical or Horizontal scan Auto Pop Up 527 Peaks Mode Category 7 Options Select Group 1 5 3 7 Elevations via overlay Manual select None Display controls selection O Manual deselect ________ None Display controls selection y O Auto Range Controlled by display response if selected 10 NM range willbeused Moving Marker Overlay Page Controlled by display 12 Display bus type 453 1 J1 59 7 2 453 2 B J1 57 72 Display Input Control Group 4 CHANNEL CONNECT TO KCPB IND Bus 1 out Fault Designation KCPB BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Tvpe Basic
91. Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Roll Angle 6 2 31 14 180 degrees Basic 0 010986328125 Pitch Angle 6 2 34 14 180 degrees Basic 0 010986328125 Body Roll Rate 6 2 50 128 deg sec Basic 0 01562500 Body Pitch Rate 6 2 49 128 deg sec Basic 0 01562500 Inertial Vertical Speed 6 2 56 32 768 Basic 1 0 Inertial Altitude 6 2 57 131 072 ft Basic 0 125 CHANNEL 429RX_7 Data Reference Signal Type Resolution Roll Angle 6 2 31 180 degrees Basic 0 010986328125 Pitch Angle 6 2 34 180 degrees Basic 0 010986328125 Body Roll Rate 6 2 50 128 deg sec Basic 0 01562500 Body Pitch Rate 6 2 49 128 deg sec Basic 0 01562500 Inertial Vertical Speed 6 2 56 32 768 fpm Basic 1 0 Inertial Altitude 6 2 57 131 072 ft Basic 0 125 Note ID 253 may only be used with Category 2 digital Barometric Altitude Rate sources analog sources are not compatible with Inertial Vertical Speed Table 5 3 10 255 Attitude Input Select Type 255 CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Roll Angle 6 2 31 180 degrees Basic 0 010986328125 10 20 Pitch Angle 6 2 34 180 degrees Basic 0 010986328125 10 20 Normal Acceleration 6 2 42 E4 g s Basic 0 000977 g s 10 20 Longitudinal Acceleration 6 2 43 4 g s Basic 0 000977 g s 10 20 Data Reference Sig Bits
92. CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Mode Range Word 2 21 155 Discrete 5 640NM Basic N A 50 CONN PIN REFERENCE NAME PN FUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 218 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 236 Collins ProLine 4 Integrated Display Configuration Group 241 Display Type jCollnsPrline4 oo Fan Mode with 60 degree limit Peaks Mode Category 7 Options Select Group 71 Manual select Select
93. Control Group 0 CHANNEL CONNECT TO KCPB IND Bus 1 out Fault Designation KCPB BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 CHANNEL CONNECT TO KCPB IND Bus 2 out Fault Designation KCPB BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed E Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x Integration Notes 1 When interfacing to a single display controller configuration the Display Input bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 KCPB Keyed Component Picture Bus is also known as ASPB AlliedSignal Picture Bus 3 Label 012 is optional The current fault and fault history message RANGE for label 271 Range
94. EGPWS requires a GPS with 8 channels minimum and RAIM capability Appendix E Table 5 3 3 defines the Position Input Select options and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry Appendix E Tables 5 3 3 x where x is the Position Input Type number define the label set and electrical interface required to support each Position Input Type GPS Input selection is available in the following formats ARINC 429 low speed ARINC 429 high speed RS 232 and Internal The Internal GPS uses ID 2 A unit equipped with an internal GPS 965 1190 XXX and 965 1220 XXX may use an external GPS source See Category 7 to select GPS Altitude Reference mean sea level or WGS 84 for ARINC 429 label 076 3 5 1 ARINC 743 Format This option provides the ability to specify the GPS input data format as ARINC 743 instead of the ARINC 743A data format For ARINC 743A the VFOM is in feet and the HFOM is in nautical miles nm For ARINC 743 both VFOM and HFOM are in meters Note Universal UNS 1 C D K M GPS only output is in ARINC 743 format 3 5 2 GPS Altitude Label 076 Reference The GPS Altitude label 076 may be referenced to mean sea level or WGS 84 Determine which reference your GPS position uses and program the GPS Altitude Reference accordingly in Category 7 Note Universal UNS 1 C D K M GPS only output the Altitude Label 076 referenced to WGS 84 3 5 3 North South East West Velo
95. FAA or other regulatory agency approval 4 6 4 Material C ost and Availability The AMERICAS ATLANTIC or PACIFIC region PCMCIA card is available at no charge to Operators Order part from Honeywell Honeywell Aerospace Airlines amp Avionics Products Toulouse Office Order Administration M S 33 Centreda Avenue Didier Daurat PO Box 97001 31700 Blagnac France Redmond WA 98073 9701 Phone 33 5 6171 0079 Phone 425 885 8719 Fax 33 5 6130 0497 Fax 425 885 8988 Vendor Name Vendor P N Description QTY UM Honeywell P N Honeywell 718 1391 xxx AMERICAS Region Card 1 EA 718 1393 Honeywell 402 6075 xxx AMERICAS Region Label 1 EA 402 6075 xxx Honeywell 718 1392 xxx ATLANTIC Region Card 1 EA 718 1392 xxx Honeywell 402 6075 xxx ATLANTIC Region Label 1 EA 402 6075 xxx Honeywell 718 1393 xxx PACIFIC Region Card 1 EA 718 1393 xxx Honeywell 402 6075 xxx PACIFIC Region Label 1 EA 402 6075 xxx 4 6 5 Accomplish ment Instructions Load the PCMCIA card data as described in paragraphs 4 6 5 A or 4 6 5 B below Loading time will be approximately 10 minutes A Loading the PCMCIA Card Data with Computer Mounted in the Aircraft 1 Connect the Smart Cable Honeywell PN 951 0386 001 to the EGPWC J3 connector 2 Ensure that the 28 VDC circuit breaker to the EGPWC in ON and that the COMPUTER OK LED on the EGPWC front panel is on 3 Insert the PCMCIA card into the Smart Cable PCMCIA card slot Proprietary notice
96. False Tm Fase Ms 00 False False F2 ras ee ee 000 01 Fase Tme Te Tm wosst 00 _ ee rue Tn 32 False True False False False False WGS 84 020 33 Ime fake f Fale Fase MSL _ False False False False WGS 84 020 mue False Flee True wi j o j False False False False False False False False False False False 8 False False 9 False False 10 False False False False 12 False False 13 False False 14 False False 15 False False 16 False 17 False 18 False 19 False 20 False 21 False 22 False 23 False 24 False 25 False 26 False Tume 27 False Tume 28 False Tue TRUE enables steep approach selection via Steep Approach Select Discrete see Section 5 3 13 and 6 6 25 2 Enables PEAKS mode display if display supports see display configuration group Section 5 3 6 3 MSL reference must be selected when an internal GPS is utilized Refer to Table 5 3 3 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 241 Honeywell MK VI MK VIII EGPWS Installation Design Guide Steep TA amp D Peaks Obstacle Bank Angle Flap GPS Altitude Software Approach
97. GPS Antenna with 26dB gain A 40 foot coax cable run with 1 coax connector at the rack disconnect The cable has a specified line loss of 0 25dB foot 118dB received signal 26dB antenna gain 92dB 10dB line loss 0 25dB foot x 40 foot run 0 6dB rack coax connector insertion loss 102 6dB at EGPWS coax connector better than required 106dB This is an acceptable installation Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 16 Honeywell MK VI MK VIII EGPWS Installation Design Guide 1 5 5 OAT Sensor The EGPWS uses a separate OAT sensor Outside Air Temperature to measure outside air temperature on aircraft that do not have another compatible source of outside air temperature Outside Air Temperature is used by the EGPWS along with pressure altitude in the Geometric Altitude computation If Outside Air Temperature is not available Geometric Altitude is computed using pressure altitude and GPS Altitude with a corresponding reduction in accuracy Honeywell engineers have determined that the reduction in accuracy is small because the GPS Altitude is the strongest element in the computation Geometric Altitude is computed by the EGPWS to reduce or eliminate errors potentially induced in corrected barometric altitude by temperature extremes non standard altitude conditions and altimeter miss sets Geometric Altitude also allows continuous EGPWS operation in QFE env
98. Gear Up 6 6 3 28V Landing Gear Discrete Type Supplied by landing gear or landing gear selector handle position sensitive switch This input can be paralleled with or used exclusively by a Gear Override Switch if an alternate source of Gear Position is used Signal Status Landing Gear Down or Landing Gear Up Fault monitoring Indication of landing gear selected for more than 60 seconds at airspeeds above 290 200 for GA Slow knots will result in a gear switch fault which will cause a GPW INOP indication Note This can be caused by either a gear switch fault or by the Gear Override switch being left in the on position Level 6 Audio readout 28 V Landing Gear Discrete Landing Gear Down gt 28 Volts Landing Gear Down Landing Gear Up gt 28 Volts Landing Gear Up Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 297 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 6 4 GND Landing Flap Discrete Type Supplied by Flap or Flap selector handle switch Signal Status Landing Flaps or Not Landing Flaps Fault monitoring Indication of landing flaps selected for more than 60 seconds at airspeeds above 250 180 for GA Slow knots will result in a flap switch fault which will cause a GPW INOP indication Note This can be caused by either a flap switch fault or by the Flap Override switch being left in the on position Level 6 Audio readout
99. HELP or to display a list of the Terminal Mode commands and their description is the preface command for entering the ID string Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 119 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 Using the Category ID s as chosen from the Appendix E refer to completed Table 5 2 create a command string with the following structure CFG gt CUW 0 15 HHHH HHHH Hl CUW lt space gt 0 is the command and version number writes the category ID s defined by version 0 definition 0 is the only version currently available to the Configuration Module via the EGPWC without a CRC checksum value attached this is generated by the EGPWC when the data is transmitted 1 15 indicates the beginning of the data string with 15 being the number of categories to follow lt gt lt 1 ID gt lt space gt lt Cat 2 ID gt lt Cat 15 ID gt each Cat ID is the chosen ID for the category from the Appendix E Table 5 2 The ending slash indicates the end of the data string Note f 15 ID s do not follow 15 the error message Invalid Parameter Not enough ID s Configuration update failed please try again will be given The value entered for each category must be an available ID for the associated category or a similar error message will be given If the number of
100. Honeywell RS 422 Serial Control Interface SCI Mode Range Word Serial Control Interface SCI Mode Range Word 1 80 Serial Control Interface SCI Status Word 1 FF Honeywell RS 232 Serial Control Interface for DC811 Up Down Range 6 6 DISCRETE INPUTS 6 6 1 6 6 2 6 6 3 6 6 4 6 6 5 6 6 6 6 6 7 6 6 8 6 6 9 6 6 10 6 6 11 6 6 12 6 6 13 6 6 14 6 6 15 6 6 16 6 6 17 6 6 18 6 6 19 6 6 20 6 6 21 6 6 22 6 6 23 6 6 24 6 6 25 6 6 26 6 6 27 6 6 28 Analog Radio Altitude Validity Flags GND Landing Gear Discrete 28V Landing Gear Discrete GND Landing Flap Discrete 28V Landing Flap Discrete Momentary Flap Override Discrete Self Test Discrete GND ILS Tuned Discrete 1 28V ILS Tuned Discrete 1 Glideslope Validity Discrete 1 GND Glideslope Inhibit Discrete 28 V Glideslope Inhibit Discrete Glideslope Cancel Discrete Decision Height Discrete Mode 6 Low Volume Discrete GND Audio Inhibit Discrete 28V Audio Inhibit Discrete Display Select Discrete 1 Display Select Discrete 2 Terrain Awareness amp TCF Inhibit Discrete Autopilot Engaged Discrete 1 Barometric Altitude Validity Discrete Magnetic Heading Validity Discrete Attitude Validity Discrete Steep Approach Discrete 2 Timed Audio Inhibit Discrete GPWS Inhibit Discrete Localizer Validity Discrete 1 7 OUTPUT DATA DEFINITION 71 ARINC 429 OUTPUT DATA 7 1 1 7 1 1 1 7 1 1 2 Discrete Output Words EGPWS Alert Discrete 1 270 EGPWC Logic D
101. Input Control Group 3 CHANNEL CONNECT TO SCI Bus 1 Fault Designation DISPLAY BUS 1 429 422RX 1 Format RS 422 12K baud Bus Tvpe Basic A J2 36 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 37 Range Mode Range Word 6 5 1 1 80 4 Discrete 2000NM Basic N A 100 CHANNEL CONNECT TO Fault Designation 429RX 3 Bus Type NeCemecton T T J CONN PIN REFERENCE NAME PIN FUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 Radar Indicator part number must end in X1X Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 212 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 14 Honeywell Bendix PPI 4A 4B without Auto Range Display Configuration Group 12 Display Type Bendix PPI 4A 4B MAP MODE V U Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Peaks Mode 5 3 7 Elevations via overlay Manual select Anytime 0 SO Manual deselect Anytime Auto Range M 14 O Moving Marker
102. KC Picture Bus KCPB with Digital Discrete Word Note 1 9 20 KC Picture Bus KCPB with Digital Discrete Word without presentation of 020 X Geometric Altitude Note 1 9 The following displays are only supported by the MK VIII 235 3 237 2 Collins WXI 701 711 PPI without Auto Range 020 x 0 6 EG 9 gt gt gt gt oo gt 39 9 Integrated with binary Peaks Collins ProLine 21 Integrated with overlay Peaks Elevation and Partial Compass 240 020 N Raster patch Note 4 Collins ProLine 21 Integrated with binary Peaks Elevation and Full Compass 020 N Raster patch Note 4 N 243 Honeywell EDZ802 EDZ603 EDZ803 non Integrated with dual SCI range Note 8 gt gt gt 44 Honeywell EDZ806 non Integrated with dual SCI range Note 8 45 Honeywell EDZ806 Integrated with dual SCI range N Z gt gt N 46 Honeywell Bendix EFIS 10 non Integrated Note 7 Z gt B Z gt 247 Collins FDS 255 2000 EGPWS controls selection 48 Honeywell Primus 1000 Integrated with overlay Peaks Elevation 2 gt N oo N Z gt 49 5 5 253 X 2 gt NIN gt Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 198 Honeywell MK VI MK VIII EGPWS Installation Design Guide Software EGPWS Application No
103. L 26 VAC Reference 1 L Alternate Mode 4B Threshold Program Pin J1 25 Air Temperature Reference 5VDC Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 131 Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name GPWS 965 0686 001 020 Signal Type Conn Pin _ S Signal Name MK VI MK VIII EGPWS Enhanced Audio Volume Control 1 Program Pin lt Analog Spare 500 Altitude Callout Program Pin lt Analog Spare Spare Discrete 28VDC Magnetic Heading Validity Discrete 28VDC Radio Altimeter Validity 28VDC Radio Altitude Validity Discrete 28VDC Glideslope Deviation Low Level Validity H 2 and Spare 1 Discrete Display Selected Discrete 2 GND Airspeed Expansion Discrete Display Selected Discrete 1 GND Decision Height DH Discrete GND DH Discrete GND Landing Gear Discrete 28VDC Landing Gear Discrete 28VDC External GPWS Audio Suppress Discrete 28VDC Audio Inhibit Discrete 28VDC ILS Backcourse Approach Selectd Discrete 126V Discrete X s38 28dise _Glideslope Inhibit Discrete 28 00 _ Ls Frequency Selected Discrete 28900 Discrete X 7 lt 2evdise 1 Tuned Discrete 24000 Powerinput 1 PWRGND X PWRH Powerinputzevoc Chassis Ground GND x J1 42 lt GND_ C Chassis Ground Barometric Altitude Rate nout BG Analogh mas A
104. MK VIII EGPWS Installation Design Guide Selects a Input Discrete Using Table 5 3 13 and any sub tables Record the Ident ID No on the space 13 Functions contained within locate the desired I O available on Ident column of this table ID Discrete type b Output Discrete Functions Selects Using Table 5 3 14 and any sub tables Record the Ident ID No on the space 14 contained within locate the desired Volume a Audio Output Level available on Ident column of this table ID type Selects Record the Ident 0 ID No on the 15 sing Table 5 3 15 select 0 Unused space available on Ident column of this a Unused table Selects Record the Ident 0 ID N 16 sing Table 5 3 16 select 0 Unused space available on Ident co b Unused table Selects Record the Ident 0 ID No on t 17 sing Table 5 3 ect 0 Unused space available on Ident column o c Unused table LIMITATIONS The described use of the configuration module provides for maximum flexibility in selection of input sensors and output behavior Every attempt has been made to avoid conflicts arising between categories and to reflect the known configurations of aircraft However in the case of input sensors it should not be construed that all combinations are valid configurations There may be configurations not supported by the EGPWS software configuration building process which
105. NALOG DC INPUT 2 FAILED ALOG DC INPUT 3 FAILED NALOG DC INPUT 4 FAILED gt future future future future Z Z ALOG DC INPUT 5 FAILED NALOG DC INPUT 6 FAILED ALOG DC INPUT 7 FAILED gt future future future ALOG SYNCHRO INPUT 1 FAILED ALOG SYNCHRO INPUT 2 FAILED NALOG SYNCHRO INPUT 3 FAILED ANALOG SYNCHRO INPUT 4 FAILED 7 1 5 2 Fault Diagnostic Word 2 351 Data Discrete Label Octal 351 Transmit Interval 1000 msec 10 el BIT NO future future future future N 5 53 WIN Re N gt gt gt gt zziz N 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 313 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 5 3 Fault Diagnostic Word 3 355 fe sss ___________ 7 1 6 Peak Binary Labels The following ARINC 429 outputs are used to provide Peak Elevations and color information for integrated displays where the EFIS outputs stroke written Peaks Elevation information on the display This label set consists of 2 labels containing upper and lower elevation color and display blanking data Each label is transmitted with two different SDI values for the captain s and first officer s display values 7 1 6 1 Peaks Upp
106. RS 422 receiver are provided at the aircraft interface connectors The RS 422 transceivers are electrically multiplexed with the RS 232 transceivers and are selected through the configuration process The third RS 422 receiver is electrically multiplexed with the ARINC 429 channel receiver The maintenance RS 232 bus is described in section 4 3 1 The specific characteristics data rate parity data bits stop bits is defined in the configuration selection see Section 5 and 6 for details RS 422 cable termination will not be required for typical applications see TIA EIA 422 B Annex A The RS 232 bus meets the characteristics specified in RS232C and supports the following characteristics Data Rate 1200 2400 4800 9600 19200 or 38400 bits Sec Parity None Odd or Even Data bits 7 or 8 Stop bits 1 2 Maximum Recommended Cable Length 15 meters Data definition Refer to Section 6 of this document The RS 422 bus meets the characteristics of TIA EIA 422 B and supports the following characteristics Data Rate 1200 2400 4800 9600 12000 19200 or 38400 bits Sec Maximum Transceivers on Bus 20 Receiver Input Impedance 12 Ko Word Frame Structure Refer to Section 6 of this document Data definition Refer to Section 6 of this document The bus speed is defined in the configuration selection see Section 5 for details Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 16
107. Radio Altitude Type 3 10 2 Decision Height Discrete Input The Decision Height discrete J1 33 Category 8 indicates to the MK VI MK VIII EGPWC whether the aircraft is above or below the selected Decision Height This discrete is typically connected to the Decision Height output on the Radio Altimeter indicator If the Minimums Minimums callout is not wanted the Decision Height discrete should be left open 3 10 3 Digital Radio Altitude Interface Cat 8 ID 2 ERA SMES MN Radio Altimeter R T ARINC 429 J A 21 hp R IX IX ARINC 429 o B 4 SS n B J1 Radio Altimeter Indicator DH wiper DH Discrete Gnd 33 DH out Digital RA vsd Vendor Model Ind DH R T R T Indicator SCALE wiper out A B Collins RAC 870 ALI 55 ARINC 429 P1 R V P1 2 P1 3 Honeywell ALA 52A B ARINC 429 MP B2 MP B3 Honeywell KRA 405B KNI 415 416 ARINC 429 P1 M A P4051 B P4051 C NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 91 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 10 4 Analog Radio Altitude Interface Cat 8 ID 0 1 3 4
108. Range Signal Type Resolution Rate ms Roll Angle 6 2 31 14 180 degrees Basic 0 010986328125 10 20 Pitch Angle 6 2 34 14 180 degrees Basic 0 010986328125 10 20 Normal Acceleration 6 2 42 12 346 0 000977 g s 10 20 Longitudinal Acceleration 6 2 43 12 4 9 s Basic 0 000977 g s 10 20 Note The output for Normal Acceleration reads 0 g s nominal when aircraft is on the ground or during unaccelerated level flight Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 254 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 11 Category 11 Heading Input Select The following table provides identification of the Heading type The entry in the Heading Input Select corresponds to a table that provides detailed information on the configuration For example the details for Magnetic Heading Input Select 0 are found in Table 5 3 11 0 In this category only the following signals are defined e Magnetic Heading e True Heading Table 5 3 11 Heading Input Select Heading Input Software EGPWS Select Effectivity Effectivity Table 5 3 11 x Analog Magnetic Heading 020 3 Wire Synchro with reference and validity discrete Digital Magnetic Heading High Speed ARINC 429 Note 2 00 i i 3 Digital Magnetic Heading and True Heading 020 X X High Speed ARINC 429 Note 2 Digital True Heading ui ARINC 429 via dual IOC buses Note 1 Digital Magnetic
109. Tables 5 3 6 3 x where x is the Output 429 Bus group number define the label set and the electrical interface supporting each Display Configuration output requirements Figure 3 8 1 is an example of single tube Wx Terrain display wiring connections 3 8 1 TAD amp TCF Selection The Terrain Clearance Floor TCF algorithm identifies premature descent for approaches regardless of aircraft configuration It creates a terrain clearance envelope around the airport to provide protection against controlled flight into terrain situations beyond that of the basic GPWS The Terrain Awareness amp Display feature consists of a Terrain Awareness Alerting feature and a Terrain Awareness Display feature The Terrain Awareness Alerting feature continuously computes terrain clearance envelopes ahead of the aircraft and issues alerts if the boundaries of these envelopes conflict with terrain elevation data in the terrain database The Terrain Awareness Display feature displays the data terrain relative to aircraft altitude Both TA amp D and TCF are Enabled for all ID s in Appendix E Table 5 3 6 except for TA amp D and TCF Disable ID 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 69 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 8 2 Terrain Dis play Configuration Group This option provides the ability to specify the type of Terrain Display compatible with the aircraft co
110. Vertical Profile Mode Some display systems support a vertical profile WXR display where the radar scans up and down This mode can not support a terrain display Therefore when this mode bit is set indicating that the profile mode is active the EGPWS is to treat this as a non displayable mode Displayable Vertical Profile On Vertical Profile Off __ 0 ____ 6 2 28 Discrete Word 275 600 onl Discrete Word IC600 Packed Discrete Word 4 LABEL Octal 275 Units N A Max Range N A Approx LSB N A Data Bits Bit 17 See TABLE N A Sign Bit N A Pad Bits N A Transmit Interval mSec 500 ms Data Type Discrete SDI Bits 9 10 BIT ASSIGNMENTS Discrete Data Bit Definition IC outputting MFD format Bit 17 1 IC Driving Display its range is displayed Bit 17 20 IC not Driving Display 6 2 29 Radio Altitude 164 Source ARINC 707 LRRA or IOC Units Feet Approx LSB 0 125 Foot Data 27 Complement Binary 6 2 30 Glideslope Deviation 174 or 117 GLIDESLOPE DEVIATION Source ARINC 710 ILS or IOC LABEL Octal 174 or 117 Units See NOTE Max Range 0 8 DDM Approx LSB 0 000195 DDM Data 17 to 28 12 Fly Down Above Beam C L Sign Bit 29 Pad Bits 11 to 16 Transmit Interval mSec 33 3 to 66 6 Data Type 2 s Complement Binary SDI Bits 9 10 NOTE Units Difference in Depth of Modulation DDM 0 0875 DDM 1 Dot Proprietary notice on title page a
111. ____ MODE4TOOLOWGEAR TOOLOWGEAR 1 MODE 4 TOO LOW FLAPS TOOLOWFLAPS gt MODE 5 GLIDESLOPE MODE 1 SINKRATE SINKRATE 5 Note The basic warning is SINKRATE PAUSE SINKRATE However if the Mode 1 Pullup curve is violated only a single Sinkrate may occur prior to the pull up voice MODE 3 DON T SINK DON T SINK PAUSE DON T SINK MODE 5 GLIDESLOPE GLIDESLOPE MODE 6 BANK ANGLE BANK ANGLE PAUSE BANK ANGLE BANK ANGLE BANK ANGLE Honeywell Algorithm at low altitudes MODE 7 WINDSHEAR CAUTION QUIET or CAUTION WINDSHEAR if Caution voice Enabled Note 1 These are the only voices that can interrupt Note 2 The preface voices will always be given prior to the warning voice Note 3 Voice message is continuous Note 4 Voice message will repeat every 10 seconds Note 5 Long Self Test will only issue a single Sinkrate Note 6 The Windshear Alerts will only be given on a MK VIII EGPWS with Windshear enabled per Category 12 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 195 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 5 2 Audio Menu Type 2 Basic for Fixed Gear Aircraft 7 WINDSHEAR WARNING _ SIREN WINDSHEAR WINDSHEAR WINDSHEAR 6 TERRAIN AWARENESS PREFACE TERRAINTERRAIN 12 2 1 2 MODE2TERRAIN TERRAIN 142 MODE 6 MINIMUMS SELECTEDCALLOUTS 12 TERRAIN AWARENE
112. a ot E E ROT PORTO DERE IET RYE uqu TETUR VINEA n u 14 135 DESCRIPTION OF EQUIPMENT aue bun ai ien a sents REPE Re 15 L5 IL ME VEEGPWS Computer i t oo otto eds 15 MK VATE EG PWS COM pater nn Ass 15 1 5 3 MK VI MK VIII EGPWS Configuration 15 1 5 4 GPS Antenna and Cabling ee esee esee E Qm a the tne n uyu a usa 16 OAT SCNSOP 2 C MAE 17 1 5 6 Smart Cable PCMCIA Interface a eerie t ER ten dne 17 1 6 TECHNICAL CHARACTERISTICS ertt n e BT re nde e ied e etri Eo P 18 1 7 UNITS SUPPLIED eret IEEE D e p ACE de 18 DSTA VRE GRASS IRAN ML deca Sa Bs Retna A e ER Ed UE 18 DET 2 MKCVIHTEGBWS i ERAT GR ERR RR EA ER 19 I3 Configuration Module ih d t eee derriere b eterne ed e teet a quq 19 1 7 4 Smart Cable PCMCIA Interface nete enne trennen rene tree rennen ener 19 1 8 INSTALLATION KITS AND ACCESSORIES nennen nennen tnit 19 1 8 1 MK VI MK VIII EGPWS Installation eene nennen nennen rhet tente trennen eere nennen een 19 1 8 2 RS 232 Cable b te Rn BO I REI RITE 20 L 5 3 5mart Cable see A 20 I 6 4 Terrain Database Cards
113. associated with each Terrain Display configuration Each of the ID rows has a group number for the Display Configuration the Input Control The TA amp D Pop Up Disable function is defined by a Boolean The ID groups will completely identify a particular Terrain Display Interface Table 5 3 6 Terrain Display Select Software EGPWS Effectivity MKVIII No Display TAD and TCF Enable 020 X TAD TCFDisaled __ 00 X Collins ProLine 4x4 Note 00 X HoneywellBendix PPI 4A 4B with Auto Range Nofe3 771 500 X Collins ProLine II 5x6 Note2 1 00 X Collins ProLine 5x4 5x5 Note2 00 X Honeywell Bendix IN182A IN812A RDR 2000 RDS 81 82 00 X Honeywell Bendix IN842A IN862A RDR 2100 RDS 84 86 00 X Honeywell Bendix EFIS 40 50 non Integrated 00 X S Application Notes P gt lt gt Honeywell Bendix EFIS 40 50 Integrated Note 6 8 020 X Collins WXI 701 711 PPI with Auto Range 020 xX PX lt gt Honeywell Bendix PPI 4A 4B without Auto Range Note 3 020 X Honeywell P880 660 440 Integrated WXPD with SCI range o X Honeywell P880 660 440 Integrated WXPD with SCI range Aircraft symbol 020 X UA gt lt gt gt Picture Bus KCPB without presentation of Geometric Altitude Note 1 020
114. bit if configured by the display type 28V_DISC_11 Not Defined in this ID Note 3 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 260 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 2 Input Output Discrete Type 2 CHANNEL CONN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE coer Sac ns umm cgo mem Inr ose hs ad Steep Approach Discrete 2 Note 2 Gnd Selected 32 31 alternate action lt not gt Gnd Not Selected J1 72 MON OUT 1 Output GPWS INOP Discrete i743 TAD INOP Discrete GPWS Warning Discrete 7 4 1 J1 78 DISC_OUT_1 Output Terrain Awareness Caution or Warning 7 4 7 1 Obstacle Awareness Caution or Warning 7 4 7 2 Guu GPs Alen Discrete Gidesope Oni us ouput Gidesape Our e pscours owu SSS ouput Terain Displey Deces Oupu 744 OOO O y __ 1 48 28V DISC 11 Input NotDefinedinthisID Note3 o J2 15 28V DISC 13 Input j NotDefindinthisID Note3 o J150 MON OUT3 Output jNotDefinedinthisID Note3 o o DISC OUT
115. buses Cat 10 ID 253 amp 255 Attitude Input Select Type 253 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 324 325 326 327 365 and 361 Attitude Input Select Type 255 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 324 325 333 and 331 For interface description see paragraph 3 4 5 Air Data Type 255 3 12 5 Instruction s Using Appendix E Tables 5 2 5 3 10 and 5 3 10 x as described above select the Attitude Input Select type that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Attitude Input Select from Appendix E Table 5 3 10 under the Ident No heading for Step Category 10 in Appendix E Table 5 2 Using the Attitude Input Select ID number from Appendix E Table 5 3 10 as x go to Appendix E Table 5 3 10 x The electrical interfaces pin outs for the Attitude Input Select Type are shown in Appendix E Table 5 3 10 x and are used to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 99 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 13 Category 11 Heading Input Select Category 11 defines the Magnetic Heading interface Appendix E Table 5 3 11 defines the Heading Input Select types and identifies the first MK VI VIII EGPWS version in which the o
116. categories provided is less than 15 e g 78 with eight ID s defined then the remaining categories 9 through 15 will be set to 0 After completing the data string as defined above and pressing ENTER the following message may appear Confirm this data reflects configuration to be programmed If the message does not appear the cursor will flash In either case it is waiting for an answer Y or N Pressing the Y or y key confirms the data and sends the data to the EGPWC to write to the Configuration Module Following the writing to the Configuration Module the EGPWC is automatically rebooted in order for the new configuration to take affect Note If when the ENTER key is pressed the question response is not given cursor just moves to the next line pressing any character key should provide the proper response Pressing the N key results in the message Command aborted No configuration module change has been made necessary revise the data to correct or change as necessary and continue as above The backspace key can be used to make corrections 5 Following the successful writing to the Configuration Module no error messages and EGPWC reboot pressing Control Z Ctrl Z restarts the WinVIEWS Terminal Mode communication 6 There are a couple ways to now confirm the Configuration Module programming with the following being the preferred As above type to restart the Configuration sub
117. dual ARINC 429Range Sweep type Auto Pop Up 537 Peaks Mode 5 3 7 select Selection is controlled by display Manual deselect Deselection is controlled by display Auto Range YeslONM 2 _____ Moving Marker Yes Honeywell type Overlay Page Yes for Peaks Elevations only located middle right side of display Display bus type Honeywell picture bus Y YU 453 1 B J1 59 7 2 a CRM CNN SEMEN 453 2 B J1 57 72 Display Input Control Group 252 CHANNEL CONNECT TO MG SG Left Bus Fault Designation EFIS BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic Note Provides range unless MG is not backing up right side see channel 3 A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 36 Range 6 2 23 050 4 4 2000NM discrete TA amp D N A 100 Both ranges on one word CHANNEL CONNECT TO MG SG Right Bus Fault Designation EFIS BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Type Basic Note Only provides range if MG is backing up right side MG input on channel 1 is primary input A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range 6 2 23 050 4 4 2000NM discrete TA amp D N A 100 Both ranges on one word Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed A J2 43 Transmits Section 7 Label sets
118. dual high speed digital ARINC 429 signal having label 320 For interface description see paragraph 3 4 5 Air Data Type 255 3 13 5 Instruction s Using Appendix E Tables 5 2 5 3 11 and 5 3 11 x as described above select Heading Input Select type that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Heading Input Select from Appendix E Table 5 3 11 under the Ident No heading for Step Category 11 in Appendix E Table 5 2 Using the Heading Input Select number from Appendix E Table 5 3 11 as x go to Appendix E Table 5 3 11 x The electrical interfaces pin outs for the Heading Input Select Type are shown in Appendix E Table 5 3 11 x and are used to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 101 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 14 Category 12 Windshear Input Select Category 12 defines the Windshear interface Appendix E Table 5 3 12 defines the Windshear Input Select options and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry 3 14 1 No Windshear Select ID 0 No Windshear for all aircraft configurations without Windshear Windshear options will be added as new installations types are propagated 3 14 2 Dual ARINC 429 BUS Cat 14 ID 253 254 255
119. dual sets of lights are used one set on each side or a combination thereof is desired For a typical example of cockpit light locations refer to Figure 2 3 For panel cutouts and assembly options see the manufacturer s specifications The following are recommended locations GPWS amp BELOW G S or PULLUP 4 GPWS These lights should be located together and in the flight crew s primary field of view This would include either the instrument panel or the edge of the glareshield GPWS FLAP OVRD Optional This light should be located in the flight crew s field of view and within reach of both crew members This light switch may be located an assembly with the GPWS and BELOW G S lights and or other EGPWS annunciators GPWS CANCLD Optional If used this light should be located within at least one crew member s field of view GPWS INOP This light should be located within at least one crew member s field of view or with other system INOP lights of similar importance It is recommended that this light not be located in the flight crew s primary field of view The reason being that in the event of a GPWS system failure at the beginning of a flight this light will remain until the problem is fixed This light may be combined with the TERR FAIL light TERR DISPLAY ON This light should be located near the associated cockpit display in the flight crew s field of view and within reach of one or both crew member
120. eq utere uapa ayauya 114 SL FOZ LEITET 114 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 50 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION III SYSTEM PLANNING 3 1 Introduction This section provides information for selecting features and wiring the electrical interfaces of the MK VI MK VIII EGPWS Appendix E Section 5 2 groups features functions into sets called Categories This document follows the Category structure of the Appendix E It provides descriptions of the features and instructions for selecting features and for determining the correct wiring Sample wiring diagrams for the most commonly used MK VI MK VIII EGPWS configurations are provided in Appendix B Make copies of Appendix E Table 5 2 to use for recording feature selections Section 6 provides a cross reference between the MK VI GPWS Classic and the MK VI MK VIII EGPWS Enhanced interfaces 3 2 System Wiring Electrical Interfaces System wiring is broken down into the following main components A Electrical Interfaces power and ground GPS Antenna Analog and Digital Inputs Discrete Inputs Serial Outputs Audio Outputs Discrete Outputs Configuration Module Many of these inputs and outputs will be defined as the Categories are selected for Configuration Module programming Appendix E Table 8 1 1 shows the typical usage for each p
121. front panel aircraft interface connectors The aircraft interface connectors are defined as P1 78 pins and P2 50 pins Section 8 identifies the connector pin assignments The signal mnemonic for each signal in Section 8 is included in the following sections synchro inputs are brought in as three or five wire devices No two wire absolute AC signals are available All analog inputs provide broken wire detection on all input signal legs Unless otherwise stated the Maximum reverse fault current is defined as the current resulting from an internal component failure with the input signal at zero volts 4 2 4 Grounds 4 2 1 1 Chassis Ground Used for redundant metal connection This pin is internally connected to DC Ground see section 4 2 1 2 Pin Assignment Signal Mnemonic J1 42 J1 53 GND 4 2 1 2 DC Ground For discrete inputs and lamp driver outputs These pins are also internally connected to Chassis Ground see section 4 2 1 1 Pin Assignment Signal Mnemonic same as 28 VDC Return J1 41 J1 61 PWR L NOTE All analog signals are differential input 4 2 2 Primary Power Input Nominal Input 28 VDC Normal Voltage Range 22 0 to 30 3 VDC Normal Surge Voltage Range 15 to 40VDC 30 mSec Abnormal Voltage Range 20 5 to 32 2 VDC Abnormal Surge Voltage Range 37 8 VDC 1sec 46 3 VDC 100 mSec Normal Frequency Range not applicable Frequency Transients not applicable Power Requirements 9 Watts No Warnings 7 Watts w
122. information Section 3 provides information and instructions for selecting required features of the EGPWS Section 4 provides Configuration Module programming instructions Section 5 provides certification requirements Section 6 provides a pin to pin comparison of the classic MK VI GPWS to the MK VI MK VIII EGPWS Appendix A Customer Worksheet Appendix B Sample Wiring Diagrams Appendix C provides WinViews operation instructions Appendix D provides Vendor Contact Information Appendix E Interface Description Document Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 13 965 1180 601 965 1180 201 965 1190 201 965 1210 201 965 1220 201 060 4199 180 060 4267 000 060 4326 000 060 4199 194 060 4314 000 060 4188 023 060 4188 038 060 4188 041 060 4167 158 060 4199 190 060 4199 182 076 4610 000 Honeywell MK VI MK VIII EGPWS Installation Design Guide 1 4 Reference Documents Following is a list of Honeywell reference documents Product Specification for the MK VI and MK VIII Enhanced Ground Proximity Warning System EGPWS Outline MK VI EGPWC without GPS Outline MK VI EGPWC with GPS Outline MK VIII EGPWC without GPS Outline MK VIII EGPWC with GPS Line Maintenance Manual MK VIII EGPWS Terrain Database Airport Coverage List 3500 Runways MK VI MK VIII EGPWS Terrain Database Airport Coverage List 2000 Runways MK VI
123. mSec 1000 Maximum Data Type 2 s Complement Binary SDI Bits 9 10 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 278 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 2 7 Latitude 110 GPS LATITUDE GPS Source ARINC 743 A GPSSU LABEL Octal 110 Max Range 180 Degrees Approx LSB 0 000172 Deg Data Bits 9 to 28 20 Sign Bit 29 Pad Bits None Transmit Interval mSec 1000 Maximum Data Type 2 s Complement Binary SDI Bits 9 10 6 2 8 Longitude 111 GPS LONGITUDE GPS Source ARINC 743 A GPSSU LABEL Octal 111 Max Range 180 Degrees Approx LSB 0 000172 Deg Data Bits 9 to 28 20 East Sign Bit 29 Pad Bits None Transmit Interval mSec 1000 Maximum Data Type 2 s Complement Binary SDI Bits 9 10 6 2 9 Track Angle 103 GPS 6 2 10 Horizontal Figure Of Merit 247 GPS ARINC 743A 6 2 11 Horizontal Figure Of Merit 247 GPS ARINC 743 6 2 12 Horizontal Figure Of Merit from HDOP 101 GPS ARINC 743 The HDOP scaling is multiplied by 16 to produce HFOM values required by the EGPWS 6 2 13 Vertical Figure Of Merit 136 GPS ARINC 743A 6 2 14 Vertical Figure Of Merit 136 GPS ARINC 743 6 2 15 Vertical Figure Of Merit from VDOP 102 GPS ARINC 743 VERTICAL FIGURE OF MERIT GPS Source ARINC 743 GPSSU LABEL Octal 102 Max Range 16 384 Approx LSB 0 5 Data B
124. mode At the gt prompt type CMR lt Enter gt Each category and its associated ID is read from the Configuration Module and listed on the PC screen Alternately when not in the Configuration sub mode the command PS lt Enter gt Present Status will display EGPWC and configuration data 7 Configuration Module programming is complete If the CFG gt prompt is still present type Exit lt Enter gt to exit the Configuration sub mode Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 120 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 5 1 CUW and CMR Commands An example CUW command data string its definition and the corresponding CMR list is provided below CUW command data string CFG gt CUN 0 15 2320039310000000 Type Y or y to confirm the data and send the data to the EGPWC to write to the Configuration Module Above configuration defined Category 1 Aircraft Mode Type 2 Category 2 Air Data Type 3 Category 3 Position Type 2 Category 4 Altitude Callouts Menu 0 Category 5 Audio Menu 0 Basic menu Category 6 Display Type 3 Category 7 Options Select Group 1 93 Steep Approach True TA amp D Alternate pop up False Peaks Mode True Obstacle Awareness True Bank Angle True Flap Reversal False GPS Altitude Ref MSL Category 8 Radio Altitude Type 1 Category 9 Navigation Type 0 Category
125. not HSI backup or SG backup AND if label 051 bit 11 transitions from 0 to 1 rising edge AND Checklist is not selected on the MFD AND TCAS Auto Pop Up is not occurring The display will change to Map mode The display will energize the Terrain selection relays The display will annunciate TERR The display will change to the range indicated by the EGPWS ARINC 429 label 050 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 237 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 253 Collins FDS 255 2000 with selection controlled by the display MK VIII Only Display Configuration Group 253 Display Type Collins FDS 255 2000 F i SwepType 4 Auto Pop Up 5 3 7 therefore enable disable of pop up is done via the display Peaks Mode select Selection controlled by display Manual deselect Deselection controlled by display Auto Range ________ see Integration Notes Moving Marker Overlay Page 7 Yes for Peaks Elevations only located on lower left of the display Display bus type Standard DISPLAY BUS 1 CONNECT TO 453 1 1 58 Terrain Display data to switching relay Symbol Generator 1 4 2 13 2 0 01 DISPLAY BUS 2 CONNECT TO E J1 56 Terrain Display data to switching relay Symbol Generator 2 4 2 13 2 Bun a 54 Display Input Control
126. on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 123 Honeywell MK VI MK VIII EGPWS Installation Design Guide NOTE Precautionary notes on the PCMCIA card regarding insertion and or removal while power is applied should be ignored since the EGPWC automatically handles the application and removal of PCMCIA card power 4 While the loading is in progress the INPROG LED on the Smart Card remains ON and the COMPUTER OK LED on the EGPWC is OFF 5 When loading is complete the XFER COMP LED on the Smart Card turns ON 6 Remove the PCMCIA card from the Smart Card slot 7 After approximately 15 seconds the COMPUTER OK LED comes ON to indicate that the contents of the PCMCIA card were successfully transferred 8 Remove the Smart Card connector from the EGPWC front panel J3 connector 9 To perform the verification of the Terrain Database version go to paragraph 4 6 6 below B Loading the PCMCIA Card Data with Computer Mounted on the Bench 1 Locate a 28 VDC Power Supply with a minimum supply current of 2 amps 2 With the Power Supply turned OFF connect the Power Supply to the J1 connector of the EGPWC as follows pin J1 53 is connected to chassis ground internally and does not need to be ground in aircraft wiring J1 connector Pin Pin Nomenclature J1 40 J1 60 28 VDC J1 41 J1 61 28 VDC J1 42 J1 53 Chassis GND Pins J1 42 and J1 53 are both connec
127. page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 202 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 4 Honeywell Bendix 4 4 with Auto Range Display Configuration Group 1 Display Type Bendix PPI 4A 4B MAP MODE V U Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Peaks Mode 5 3 7 Elevations via overlay Manual select Anytime 0 SO Manual deselect Anytime Auto Range YeslONM 2 Moving Marker 2 SO Overlay Page Without Peaks TERR located in the lower right corner With Peaks Peaks numbers located in the lower right corner Display bus type ARINC453 Ba QUIC i ii i 453TX 1 A J1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 2 22 DISPLAY BUS 2 CONNECT TO aa 1 57 72 Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Display Word 2 6 2 20 271 Discrete 5 320NM Ba
128. state discretes 2 13 Open 28VDC two state discretes The EGPWS supports the following inputs in discrete form The Level 6 audio information specifies the voice issued when a state change occurs on the input discrete during level 6 self test Refer to the Product Specification for self test description 6 6 1 Analog Radio Altitude Validity Flags A Radio Altitude Validity Flag is used by the EGPWS for analog Radio Altimeter inputs Type Validity from ARINC 552 ALT 55 Radio Altimeter or RT 200 300 analog Signal Status Valid or Invalid Level 6 Audio readout Valid gt Radio Altimeter 1 Valid Radio Altitude Validity Discrete Invalid gt Radio Altimeter 1 Invalid 6 6 2 GND Landing Gear Discrete Type Supplied by landing gear or landing gear selector handle position sensitive switch This input can be paralleled with or used exclusively by a Gear Override Switch if an alternate source of Gear Position is used Signal Status Landing Gear Down or Landing Gear Up Fault monitoring Indication of landing gear selected for more than 60 seconds at airspeeds above 290 200 for GA Slow knots will result in a gear switch fault which will cause a GPW INOP indication Note This can be caused by either a gear switch fault or by the Gear Override switch being left in the on position Level 6 Audio readout Landing Gear Discrete Landing Gear Down gt Landing Gear Down or Gear Override Landing Gear Up gt Landing
129. that there is adequate space in the front of the computer for connectors and cabling B Referto Figure 2 2 and 2 3 for outline dimensions of the computer and mounting tray Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 30 Honeywell MK VI MK VIII EGPWS Installation Design Guide Mount the EGPWS mounting tray in the aircraft radio rack or other location using the four screw mounting holes Match drill the mounting holes using the Mounting Tray as a template Ensure that the mounting tray is electrically bonded less than 10 milli ohm to aircraft ground Slide the EGPWS unit in the mounting tray and secure it using the Hold Down latch After Continuity and Power check Attach the cable harness to the front panel connectors and lock connectors using the slide lock of the P1 amp P2 connectors The EGPWS should be wired according to the interconnect diagrams in Section III of this manual 2 3 4 Configurati on Module Location The aircraft configuration is programmed into the EGPWS Configuration Module installed in the aircraft wiring The Configuration Module is identified as Honeywell part number 700 1710 020 optional part number 700 1710 001 The Configuration Module is installed as one side of the P2 50 pin mating connector backshell and contains electrically reprogrammable memory for configuration storage The Configuration Module when installed is wired directly to th
130. title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 292 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 3 2 Uncorrected Barometric Altitude 203 UNCORRECTED BAROMETRIC ALTITUDE Source ARINC 575 ADC LABEL Octal 203 Max Range 131 072 Feet Approx LSB 1 Foot Data 13 to 29 17 Above Sea Level ASL Sign Bit Part of SS Pad Bits 9 to 17 Transmit Interval mSec 62 5 Maximum Data Type 2 s Complement Binary SDI Bits N A 6 3 3 Barometric Altitude Rate 212 Approx LSB 10 Ft Min 6 3 4 Computed Airspeed 206 6 4 Digital Data RS 232 RS 232 data can be received and transmitted from an internal GPS Pxpress card in TTL voltage level for use as a GPS source This data can also be received from a simulator in a TIA EIA RS 232 format which will be emulating the GPS data format of the GPS Pxpress card The characteristics of the GPS Pxpress data is 9600 baud 1 stop bit 8 bit data odd parity 6 4 1 Xpress GPS Packets ID 15 Lat Lon Estimated Horizontal Position Error O ValidFlag Valid l Invaid O Horizontal position error 2 standard deviation of horizontal position 6 4 2 Xpress GPS Packets ID 16 Altitude Estimated Vertical Position Error 0 ValidFlag Valid l Invalid O Altitude is MSL Altitude which is computed from WGS 84 altitude by adding the geoid correction Vertical position error 2 standard d
131. will cause the EGPWS to fail in an obvious manner In general you can not have redundancy through the mixing of analog and digital sources however redundant digital signals on different buses are permissable As it is not practical to verify all possible sensor combinations verification of particular sensor combinations is part of the installation certification process If you intend to implement a sensor configuration not currently identified in Section 5 please contact Honeywell or an authorized dealer installer Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 176 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 Configuration Selection Tables Configuration selection is defined by category or group of functions or inputs The Category number identifies the subsection where the details are defined For example Air Data Category 2 is defined in Section 5 3 2 and Position Input Source Category 3 is defined in Section 5 3 3 5 3 1 Category 1 Aircraft Mode Type Select In this category the following parameters are defined e Basic mode alert thresholds Selected Mode 4B threshold Selected airspeed expansion Landing gear type Aircraft category GA Fast GA Slow or Bizjet defines the expected aircraft models which the Aircraft Type will be allocated to It should be noted that the term GA when referring to GA Fast and GA Slow refers to Turboprop aircraf
132. 0 Attitude Input Select Category 10 defines the Roll Angle interface Appendix E Table 5 3 10 defines the Attitude Input Select type and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry Appendix E Tables 5 3 10 x where x is the Attitude Input Select Type number define the format and electrical interfaces required to support each Attitude Input Select Type 3 12 1 Roll Angle Roll Angle is used for Bank Angle callout and Terrain Awareness display Each leg of the Roll Synchro is required The sign is used to determine left right wing down This input improves the TAD look ahead algorithm 3 12 2 Analog Pitch amp Roll Angle Synchro Cat 10 ID 0 2 4 EGPWS MK Vertical Gyro VI MK VIII X X X Roll Synchro lt Y X Y Roll Angle 2 T Z x X X Pitch Synchro lt Y X Y Pitch Angle 2 cy 2 Attitude Validity 28 Valid Analog VG vsd Vendor Model Attitude Pitch Synchro Note 1 Roll Synchro Note 1 Vertical Gyro Valid 28 x Y 2 Y 7 Aeronetics RVG 801 P1 U 1 P1 F Collins 85 P1 13 2 43 P2 44 Collins 3320 11 1 1 P1 B P1 C P1 E P1 F Honeywell 01075 J1B G3 J1B D10 J1B D11 Honeywell HG1095 J1B G3 J1B D10 J1B D11 JET VG 208 P1 U P1 A P1 B P1 C P1 E P1 F King KVG 350 GG FF Q R Litef LTR 81 MP A11 MP B5 MP B6 Litef LCR 92 amp 93 Note 2 J3
133. 0 Auto Range Yes 10 Moving Marker Yes Honeywell type 22 5 Auto Pop Up Category 7 Options Select Group 1 5 3 7 Overlay Page Yes for Peaks Elevations only located middle right of display Display bus type Honeywell picture bus DISPLAY BUS 1 CONNECT TO 453 1 1 58 Terrain Display data to switching relay Symbol Generator 1 left channel 4 2 13 2 J1 59 7 2 DISPLAY BUS 2 CONNECT TO 453TX 2 A J1 56 Terrain Display data to switching relay Symbol Generator 1 and right channel 4 2 13 2 J1 57 722 Display Input Control Group 249 CHANNEL CONNECT TO SCI Bus 1 Fault Designation DISPLAY BUS 1 Format RS 422 12 0K baud Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms 2 37 Range Mode Range word 6 5 1 1 80 4 discrete 2000NM Basic N A 100 Status 6 5 1 2 FF Discrete N A Basic N A 100 CHANNEL CONNECT TO SCI Bus 2 Fault Designation DISPLAY BUS 2 2 10 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms Range Mode Range word 6 5 1 1 80 4 discrete 2000NM Basic N A 100 Status 6 5 1 2 FF Discrete N A Basic N A 100 Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x J2 42 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 The DIS
134. 0 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 Discrete Word 6 2 55 Discrete N A Basic N A 200 CHANNEL CONNECT TO KCPB IND Bus 2 out Fault Designation KCPB BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms 12 41 Range 6 2 35 11 0 5 1023 5NM Basic 0 5 250 B J2 40 Query Continuous Response 6 2 24 Discrete N A Basic N A 1000 DSU Status Data DSU only 6 2 36 Discrete N A Basic N A 1000 Key Press Display Mode 6 2 25 Discrete N A Basic N A 250 Discrete Word 6 2 55 Discrete N A Basic N A 200 Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed 12 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x J2 42 Integration Notes 1 When interfacing to a single display controller configuration the Display Input bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 KCPB Keyed Component Picture Bus is also known as ASPB AlliedSignal Picture Bus 3 Label 012 is optional The current fault and fault history message RANGE for label 271 Range is not shown if Range Keys are requested on label 012 Key Press Display Mode 4 The Display group is configured by the Display using response la
135. 0 feet above the ground 200 Mode 4B The voice Too Low Flaps is intitiated at 200 feet above the ground e Normal Alternate Airspeed Expansion are described as follows Normal Airspeed Expansion e Above 178 knots penetration of the Mode 4 envelope will cause a Too Low Terrain voice e Below 178 knots penetration of the Mode 4 envelope will cause a Low Gear voice Alternate Airspeed Expansion e Above 148 knots penetration of the Mode 4 envelope will cause a Too Low Terrain voice e Below 148 knots penetration of the Mode 4 envelope will cause Low Gear voice Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 177 Honeywell MK VI MK VIII EGPWS Installation Design Guide The following table provides identification of the basic Aircraft Mode Types and associated parameters For purposes of selecting an ID use the Description provided in Table 5 3 1 appropriate to the desired variables as given above Table 5 3 1 Aircraft Mode Type Select Aircraft Software Mode DESCRIPTION Effectivity Type GA Fast Fast Turboprop Slow Turbofan 170 Mode 4B Normal Airspeed Expansion GA Fast Fast Turboprop Slow Turbofan D 020 150 Mode Normal Airspeed Expansion 1 200 Mode 4B Normal Airspeed Expansion 020 GA Slow Slow Turboprop 020 170 Mode 4B Alternate Airspeed Expansion GA Slow Slow Turboprop
136. 00 Parity None Data bits 8 Stop bits 1 Maximum Recommended Cable Length 15 meters Pin Assignment Signal Mnemonic Transmit J3 4 RS232TXD_MON Receive J3 3 RS232RXD_MON Common J3 1 GND 4 3 2 PCMCIA SmartCable Port One port is provided which meets the Motorola SPI characteristics The PCMCIA SmartCable interface allows for both the uploading and downloading of internal MK VI and MK VIII EGPWS information Using this interface system software and databases can be updated Control of the upload download process 1s accomplished by connection of the SmartCable to the MK VI or MK VIII EGPWS front panel test connector and insertion of the PCMCIA card LEDs are provided on the SmartCable for PCMCIA interface operation The PCMCIA SmartCable is not intended as on line in flight storage medium and must be removed after completion of the upload download operation Electrical Characteristics Refer to the Motorola SPI specification Data definition Refer to the Motorola SPI specification Maximum Recommended Cable Length 2 meters Pin Assignment Signal Mnemonic Clock J3 7 SPICLK Master Data Out J3 9 SPIMOSI Master Data In J3 8 SPIMISO SmartCable Select J3 10 SPISEL SCZ SmartCable 5 VDC J3 6 SC_PWR SmartCable 5 VDC Return J3 1 GND PCMCIA Card Present J3 2 CARD_PRES SmartCable Ground J3 12 13 14 GND NOTE SmartCable 5VDC Return is common with RS 232 Maintenance Port common 4 3 3 GSE Present Discret
137. 000172 Basic 0 00000008381903 000 0 000172 Basic 0 00000008381903 000 32768 Basic 1 000 16 nm Basic 0 00012207 000 131 072 ft Basic 0 125 000 32768 ft Basic 0 125 000 16nm Basic 0 000061035 000 4096 Knots Basic 0 125 000 180 Degrees Basic 0 005493 1640625 000 Discrete Wd Basic n a 000 Discrete Wd Basic 0 1 min 000 Discrete Wd Basic 1 day Longitude Fine 6 2 60 Vertical Velocity 6 2 58 GPS Hor Int Limit 6 2 5 Altitude 6 2 4 VFOM 6 2 13 HFOM 6 2 10 Ground Speed 6 2 6 True Track Angle 6 2 9 Sensor Status 6 2 16 UTC 6 2 17 Date 6 2 18 Slowest acceptable update rate in milliseconds This label is not required Data used if present N NO NO NO QA QA OO OO tA Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 191 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 3 255 Position Input Type 255 Dual High Speed ARINC 743A GPS CHANNEL CONNECT TO GPS 1 ARINC 743A Fault Designation GPS BUS 1 429RX 4 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 180 Degrees Basic 0 00017166137695 000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 000 Altitude 6 2 4 131 072 FT Basic 0 125 000 VFOM 6 2 13 32768 ft Basic 0 125 000 HFOM 6 2 10 16 Ba
138. 0773 System Retrofit with binary peaks elevations Sweep Type __ Homywel Auto Pop Up Category 7 Options Select Group 71 5 3 7 TA amp D Alternate Pop Up False amp Alternate Pop Up True therefore enable disable of pop up is done via the display Peaks Mode 53 7 Binary Peaks Elevations Yes Data passed by ARINC 429 Labels 0llandO12 7 Manual select Selection is controlled by display Manual deselect Deselectionis controlled by display 22 O Auto Range _ YeslONM Display Priority Standard Display bus type Honeywell picture bus DISPLAY BUS 1 amp 2 CONNECT TO 453TX_1 J1 58 Honeywell left right interleaved picture bus to MFD and PFD 4 2 13 2 J1 59 uu 2 CONNECT TO Not supported for this display type Display Input Control Group 250 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms FWC amp GP discrete word 6 2 48 Format 1 Typel Basic N A 100 Bits 15 18 2000NM Bits 25 28 Discrete Data Reference Sig Bits Range Signal Type Resolution Rate ms FWC amp GP discrete word 6 2 48 Format 1 Typel Basic N A 100 Bits 15 18 2000NM Bits 25 28 Discrete Output 429 Bus Group 0 CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Ba
139. 0NM Format as follows 0 10 0 U MG Note Range is on one of two buses depending on whether MG is backing up right side DISPLAY RANGE BIT ASSIGNMENTS Bits 14 11 DEFINITION Bits 14 11 DEFINITION Bits 18 15 Bits 18 15 2 1000 1001 1010 1011 1100 1101 1110 6 2 24 Query Continuous Response 011 KCPB QUERY CONTINUOUS RESPONSE Source KCPB Display LABEL Octal 011 Units N A Max Range N A Approx LSB N A Data Bits Discrete word Sign Bit N A Pad Bits None Transmit Interval Prompted Response or Data Type Discrete SDI Bits N A Continuous Response 2 30 words sec Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 283 Honeywell MK VI MK VIII EGPWS Installation Design Guide Label 011 communicates the response to the KCPB Query Setup Label KCPB Label 027 or on a continuous basis For a detailed description of the Query Continuous Response Label 011 definition see the EGPWS Interface Methodology 060 4303 000 6 2 25 Key Press Data 012 KCPB KEY PRESS DATA LABEL Octal 012 Units N A Max Range N A Approx LSB N A Data Bits Discrete word Sign Bit N A Pad Bits None Transmit Interval mSec 180 Data Type Discrete SDI Bits 0 TDU FMS key press data will be transmitted using Label 012 The state of the front panel keys will be transmitted nominally every 180 ms Keys which
140. 1000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 1000 Sensor Status 6 2 16 Discrete Wd Basic n a 1000 UTC 6 2 17 Discrete Wd Basic 0 1 min 1000 Date 6 2 18 Discrete Wd Basic 1 day 1000 Notes Slowest acceptable update rate in milliseconds This label is not required Data used if present Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 190 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 3 13 Position Input Type 13 High Speed ARINC 743 GPS no N S E W Velocities CHANNEL CONNECT TO GPS ARINC 743 Fault Designation GPS BUS 429RX 4 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 1000 Altitude 6 2 4 131 072 FT Basic 0 125 1000 VFOM 6 2 14 1024 meters Basic 0 03125 1000 HFOM 6 2 11 1024 meters Basic 0 03125 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125 1000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 1000 Sensor Status 6 2 16 Discrete Wd Basic n a 1000 UTC 6 2 17 Discrete Wd Basic 0 1 min 1000 Date 6 2 18 Discrete Wd Basic 1 day 1000 Notes Slowest acceptable update rate in milliseconds This label is not re
141. 158 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX E Interface Description Document 1 INTRODUCTION 1 1 Part Number This document is the Interface Description Document for the MK VI and MK VIII Enhanced Ground Proximity Warning System EGPWS The EGPWS computer EGPWC for these systems are identified by Honeywell part numbers 965 1180 0 MK VI EGPWC With upgraded CPU 965 1190 0 MK EGPWC With upgraded CPU and internal GPS 965 1210 MK VIII EGPWC With upgraded CPU 965 1220 0XX MK VIII EGPWC With upgraded CPU and internal GPS Differences where they exist between the different part numbers are highlighted within this document The EGPWC 10 digit part number will identify the configuration of the EGPWC as follows 965 1ABC DDD example 965 1180 020 1 MK VI or2 MK B Functionality of hardware with or without internal GPS or Upgraded CPU Refer to part number list above for details VI or MK VIII EGPWC hardware including boot code C 0 as hardware part numbers roll DDD Application Software including Configuration Software The Terrain Database including the Envelope Modulation Database Version is not identified in the 10 digit part number but with a separate identifier on the nameplate All modification changes not affecting form fit or function will be identified via mod dots The digits identifying the Application software will match the respective versi
142. 19 2 Q tput Discretes 108 3 15 2 1 Lamp Format 3 15 2 2 Flashing ies eae eee ee d e eer re 109 3 152 3 GPWS Discrete T a ma a uQ dept a 2 2 0445 109 3 15 2 4 TAD INOP Discrete n 109 31525 GPWS Warning Discrete ee Oe den ede ede ddr dee 109 3 152 6 GPWS Alert Discrete n oed Led ode ed i edad tiet tege rien 110 3 15 2 7 Glideslope Cancel d Discrete seii e rinkiri at coena debe E EAE EE ERE 110 3 15 2 8 Flap Override Discretes sainia arseeni s enS AEA EOE ASNES ASERNES ESTA OATES ESSAAT nAn CAES as An E 110 3 15 29 Steep Approach Discrete sieran e d db e e d e e e ds 3 15 2 10 Audio On Discrete TCAS TAS Inhibit 3 15 2 11 Terrain Display Select 1 amp 2 Discrete 3 15 2 12 Terr m Pop up Discrete 2 2 sana aq i a DANSE UCU ONS Sih L dra Sa 3 16 CATEGORY 14 AUDIO OUTPUT LEVEL u nsn sesenta ene eee peek eae ea 341651 eec rc peel ime tos 3 17 CATEGORY 15 17 UNDEFINED INPUT 5 2 114 3 1 74 Undefined Input Select au o eter
143. 2 58 59 31 56 57 49 remove the 70 ohm termination at that MFD To allow proper radar termination when EGPWS is passing through the relays the radar picture bus has a 70 ohm resistor added externally 1 MFD P1 EHI 8D H ARINC 453 c7 11D L unterminated 10D L 70 ohm terminated EZ gt 28 1 WXR P1 P 14 ARINC 453 OUT 29 L 2 MFD P1 70 LOA 8D H ARINC 453 lt 111D unterminated 10D L 70 ohm terminated Z 28VDC Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 84 Honeywell MK VI MK VIII EGPWS Installation Design Guide 208 0072002 Nd QNO A8C geq jenas epey NI 5 AYNLOld Z geq jeues HOJIVHJN3O9 5 LHOIY QNO uognqusnd geq jeues 1ejoJ1uo HJTIOHINOO AV 1dSIG LH9I OGA 82 SIJ3 H OGA 82 8149 sng sng jo3uo2 5143 19614 149 491 pl lus sng sng sng euo fiy nbiq 0 800 0s9 NM 39NVH 39NVH IOS LY IOS 11 eve Ql 9 LYO LOATAS 109138 AN T2 14 AV T3 L1 124145 109138 dsid 14 dsid 11 dOd 2 SNE i sng Avidsia Avldsia 020 21 596 SMd93 IIIA dl
144. 2 055 EGPWS ASCII characters are not used Green TERRAIN on PFD and MFD by EFIS Label 274 If bit 13 or 22 1 then display red PULL UP on left and right PFD If bit 12 or 23 1 then display amber GND PROX on left and right PFD If bit 14 1 then display white GPWS FAIL message on PFD If bit 15 1 then display red WIND SHR message on PFD If bit 17 1 then display white WNDSHR FAIL message on PFD If bit 18 1 then display amber WIND SHR message on PFD If bit 24 1 then display amber TERRAIN FAIL message on PFD and MFD If bit 27 1 then display amber TERRAIN NA message on PFD and If bit 28 1 and display configured for Pop Up on pilots side then Pop Up Terrain on left If bit 29 1 and display configured for Pop Up on copilots side then Pop Up Terrain right If bit 14 bit 17 and bit 24 1 then display amber EGPWS SYS FAIL on PFD in lieu of GPWS FAIL and WNDSHR FAIL messages on PFD If bits 30 and 31 01 Functional Test then display white TERRAIN TEST on PFD and MFD Terrain can be displayed on the PFD and MFD Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 233 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 251 Honeywell Primus EPIC CDS R with binary Peaks Elevations MK VIII Only Display Configuration Group 251 pee c queue pem q
145. 2 1 896 IIIA 1 JO 020 0 L 1 996 IA AN no dONI ureue L INO Z O9PIA INO Lit O9PIA ddA ul zit ONINV ul ONINV SMd94 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 75 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide snuulJ 088 099 077 GL vE OOLLOOZ ull ling 899S ees 88 099 Obt IM poe1eJ6e1u Joyeoipu Jepey ll A uoH pue 104 Ps 088diul JON sng due Agz 1591 dwe sng YMd SMd93 A82 9 XVX 007 2007 088 099 Ott IM SMd93 N d sng N d sng IOS 088 099 XYM JO 700 9X21 S96 IIIA MIN 1 JO 700 9X1 1 996 IA no dONI uresa L ano Ke dsiq ul ejdsiq g V INO Z O9PIA Sr ONIHV g V INO L O9PIA ONIHV 8 V zi eBuey g V Ul L jeues ZZp SU SMd94 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 76 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide 000
146. 2 9 North South Velocity 6 2 53 East West Velocity 6 2 54 Vertical Velocity 6 2 58 Sensor Status 6 2 16 UTC 6 2 17 Date 6 2 18 NO Un Un tn CA OO Notes y Slowest acceptable update rate in milliseconds This label is not required Data used if present Table 5 3 3 1 Position Input Type 1 Low Speed ARINC 743 GPS CHANNEL CONNECT TO GPS ARINC 743 Fault Designation GPS BUS 429RX 4 Format ARINC 429 Low Speed Bus Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 1000 Altitude 6 2 4 131 072 FT Basic 0 125 1000 VDOP 6 2 15 1024 Basic 0 03125 1000 HDOP 6 2 12 1024 Basic 0 03125 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125 1000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 1000 North South Velocity 6 2 53 4096 Knots Basic 0 125 1000 East West Velocity 6 2 54 4096 Knots Basic 0 125 1000 Vertical Velocity 6 2 58 32768 fpm Basic 1 1000 Sensor Status 6 2 16 Discrete Wd Basic n a 1000 UTC 6 2 17 Discrete Wd Basic 0 1 min 1000 Date 6 2 18 Discrete Wd Basic 1 day 1000 NO NO NO Un QA QA CA CA Notes T Slowest acceptable update rate in milliseconds This label is not required Data used if present Table 5 3 3 2 Position Input Type
147. 20 x 5 3 17 Category 17 Undefined for this software release The following table provides identification for a future undefined input select category The entry in the following undefined Type corresponds to a table that will provide detailed information on the configuration The details for Undefined Type 0 are not detailed Table 5 3 17 Undefined Type Undefined Description Software Type Effectivity N A 020 x Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 269 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 CONFIGURABLE INPUT DATA DEFINITION This section defines the EGPWS input signal characteristics or data word formats for input signals commonly used in MK VI and VIII EGPWS applications See Section 5 for specific information on signal usage 6 1 Analog Input Data 6 1 1 ARINC 552 Radio Altimeter Reference Reasonable Rang Scale For Radio Altitude X 480 feet Voltsin 0 02 RALT f 0 4 For Radio Altitude gt 480 feet f f RALT f 20 Voltsi 10 1 Ln zu External Validity Flag Connection J1 29 External Validity Type 6 1 2 ALT 55 Radio Altimeter Data Item Signal Name AIC Algorithm Signal Dynamic Range Reference Dynamic Range None Reference Reasonable Range For Radio Altitude lt 500 Feet lt 10 4 VDC Volts 0 02 RALT 0 4 or RALT ft
148. 21 1 9 4 Annunciators amp Switch Annunciators 22 1 9 3 Cockpit Speakers 23 1 9 6 Temperature Probes riire labe ect oer n a ene 23 TOOESREQUIRED 46 24 1 10 1 Crimping Tool PIP2 P3 schede toe ete odit 24 TI02 Contact Positioner P3 iss tete delevi utet decere etes e este 24 1 10 3 Insertion Removal Tool P1 P2 P3 vicccccccccccccccccccccccccssessssssecccessessssssesccscsesssssceccussesssaesesecesseesessssssececeesessaseess 24 1 10 4 Spare Connectors and Contacts P1 P2 P3 a eene neret ener ener enne 25 LTT LICENSE REQUIREMENTS sasa tte o ae ee enm rn n e nei reden 25 SECTIONE INSTALLATION eerte rote qaqas cesses ses Sek e baee eus Sek ere SEE n 29 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 5 Honeywell MK VI MK VIII EGPWS Installation Design Guide ZL IN BRODUCKIONG 5 6 one metet eant etic acest mane mts 29 2 2 UNPACKING AND INSPECTING THE 220 eene e enne nennen nennen nennen ener eene nne 29 2 3 EQUIPMENT INSTALLATION ether irs ad ibit redire tefie 29
149. 2448 28V DISC 11 Input NotDefinedinthisID Note3 o J2 15 28V DISC 13 Input j NotDefinedinthisID Note3 T o J150 MONOUTS3 Output jNotDefindinthisID Note3 T o DISC OUT 7 Output NotDefinedinthisID Note3 od Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word bit if configured by the display type Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 262 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 4 Input Output Discrete Type 4 CHANNEL CONN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE coer sss umm cgo mem BENI TANTUM TII E o Se emm Tun woxowri owu wopo ha EA DISC OUT 3 Glideslope Cancel Discrete J1 73 DISC OUT 4 Output Flap Override Discrete J1 69 DISC OUT 5 Output Audio On Discrete J1 54 DISC OUT 6 Output Terrain Display Select 1 Discrete j Terrain Awareness Caution or Warning _ 1 51 DISC_OUT_8 Output Obstacle Awareness Caution or Warning 7 4 7 3 Gnd Terrain Pop Up J1 49 DISC_OUT_9 Output Terrain Display Select 2 Discrete o E J1 48 28V_DISC_11 Not Define
150. 29 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 Display channels 1 and 2 are multiplexed on ARINC 453 bus 1 3 The system only has one range for terrain display therefore the range to use depends on the value of label 275 bit 17 8 The Terrain display will Pop Up in response to EGP WS label 274 bit 28 Left display and bit 29 right display 9 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 10 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGPWS Self Test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 231 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 249 Honeywell Primus EPIC CDS R Integrated with overlay MK VIII Only Peaks Elevations Display Configuration Group 249 Function Reference section Display Type Honeywell Primus EPIC CDS R Control Display System Retrofit with overlay Peaks elevation Sweep Type Honeywell zl Auto Pop Up Category 7 Options Select Group 71 5 3 7 TA amp D Altern
151. 29 format Computed Airspeed in ARINC 575 or ARINC 429 format TABLE 5 3 2 AIR DATA INPUT SELECT E Software Description Effectivity EGPWS i e CIC 04077 1 Bendix KDC 281 i e Collins ADC 80 81 82 i e Collins ADS 65 MKVI MKVIII 1 CIC 02702 1 e Bendix KDC 481T EN TEST RENE i e Honeywell AZ 810 Digital ARINC 429 and 5000 OAT i e Shadin 2000 Analog Uncorrected Baro altitude and 5000 11 1 Honeywell AZ 241 AZ 242 AZ 648 AZ 800 020 X X AZ 810 Note 2 Analog Uncorrected Baro altitude without temperature 12 1 Honeywell AZ 241 AZ 242 AZ 648 AZ 800 020 X X AZ 810 Note 2 without temperature Digital ARINC 429 via dual IOC buses 020 N A x Note 1 Note 1 ID 255 may only be used in conjunction with other IOC bus selections for categories 6 8 9 10 11 and 12 Note 2 The AZ 800 provides an OAT signal with reference provided by the ADC This signal is not compatible with any current EGPWS interface The AZ 241 does not provide an OAT interface The installer may either add an OAT probe ID 11 or use the internal constant ID 12 Honeywell recommends ID 11 added OAT probe be used when operating in temperature extremes 0 N 3 B Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 179 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 0 AIR
152. 3 6 Smart Cable PCMCIA Interface a e acte ptite ee te BA e Raa Rane 17 T 6 TECHNICAL CHARACTERISTICS eite Ie tete I et qt ee eet Ted S m Eden etre ran 18 SUPPLIED 2 Ee De ta e T Re Rt i t aere 18 ZAMKE VIE GPW S o e pe Cae Re a ee tee 18 T 2 MK VIIPEGPMS teu eroe renta eet opem cea uns D RIEN HERE 19 127 3 Configuration Module a a ran dde tr eH u D naw na 19 1 7 4 Smart Cable PCMCIA Interface ua nala a au huan ai a retener trennen trennen ener 19 1 8 INSTALLATION KITS AND 55 5 19 1 8 1 MK VI MK VIII EGPWS Installation Kits 19 TEZ R8 232 Cable tee eremo acs ances aaah akka ehh 20 1 6 3 mart Cable Oe 20 I6 TerrainDatabase Cards au a ettet rd eara tra S au m Sesal 20 1 5 Right History Garda dee 20 F9 ACCESSORIES NOT SUPPLIED ap R ERE D a aap anu p EE ung a 20 L9 ARINGAD3 Terrain Display Wirt Ges u l Q l u aula Qu tS nu wi t haqa a 20 P SSdniennase Cable ub ei 21 Becks
153. 3125 0 00009765625 Resolution 33 3 66 6 33 3 66 6 Rate ms 6 2 30 6 2 33 Proprietary notice on title page applies CAGE COD E 97896 117 116 SCALE NONE SIZE A DWG NO 060 4314 150 REV 0 8 DDM 0 4 DDM Basic Basic 0 0001953125 0 00009765625 SHEET 251 33 3 66 6 33 3 66 6 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 10 Category 10 Attitude Input Select The following table provides identification of the Attitude Roll Angle type The entry in the Attitude Input Select corresponds to a table that provides detailed information on the configuration For example the details for Attitude Input Select 2 are found in 5 3 10 2 In this category only the following signals are defined Roll Attitude Pitch Attitude Roll Rate Pitch Rate Normal Acceleration Longitudinal Acceleration Inertial Vertical Speed Inertial Altitude Table 5 3 10 Attitude Input Select Attitude Input Description Software EGPWS Select p Effectivity Effectivity Table 5 3 10 x Analog Roll without validity 3 Wire Synchro 020 i Analog Pitch and Roll 3 Wire Synchro 020 0 C ___2 __ _____ 4 4 Analog Roll with validity 3 Wire Synchro 020 X Digital Pitch and Roll 400 ARINC 429 High Speed Note 2 Lx Digital Pitch Roll and Vertical Speed m NN ARINC 429 High Speed Note 2 x x x Digital Pitch Roll Vertica
154. 4 150 REV SHEET 66 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 6 Category 4 Altitude Callouts Category 4 defines the Altitude Callout menu choices and Smart 500 Callout selection Appendix E Table 5 3 4 defines the Altitude Callout Menu options and identifies the first MK VI MK VIII EGPWS version in which the option was available see the Effectivity entry The Altitude callout menus have selected combinations of Minimums Minimums Minimums 1000 Smart 500 500 500 Above Field 400 300 200 100 50 40 30 20 and 10 No altitude callouts may also be selected The Altitude Callout menu provides altitude annunciation for descent below predefined altitudes example One Hundred is annunciated when descending through 100 feet radio altitude A 500 foot callout is available that will issue a 500 callout once during each approach when the aircraft is 500 AGL A Smart 500 foot callout is available that will issue a 500 callout when the aircraft is 500 AGL This callout is active only during non precision approaches or when the Glideslope or Localizer deviation is greater than 2 dots 500 Above Field callout will be annunciated once during each approach when the aircraft is within 5 nm of a runway in the database and descends through 500 ft above that runway It compares the GPS based
155. 4 P2 F P1 L P1 K P1 J Sperry DG 207 J1 B 1 5 J1 M P1 L P1 K P1 J Note 1 contact the manufacturer s customer service to confirm your installation Note 2 See LCR installation manual 1 1 Heading Output Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please SHEET 100 Honeywell MK VI MK VIII EGPWS Installation Design Guide 2 2 Heading Output 3 Do not use 2 output reserved for autopilot only Note 3 The KI 525 must have the proper mod for HEADING TRANSMITTER output The Heading valid output at J2 P needs to be converted from ground active output to 28V active output using a external relay for use with EGPWS 3 13 3 Digital ARINC 429 AHRS Input Cat 11 ID 2 amp 3 Heading Input Select Type 2 AHRS bus or equivalent is a high speed digital ARINC 429 signal having label 320 Heading Input Select Type 3 AHRS bus or equivalent is a high speed digital ARINC 429 signal having labels 320 and 314 For interface description see paragraph 3 12 3 Attitude Input Type 5 3 13 4 Digital ARINC 429 Dual buses Cat 11 ID 254 amp 255 Heading Input Select Type 254 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having label 314 Heading Input Select Type 255 IOC bus or equivalent is a
156. 429 Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range 6 2 20 273 N A 5 320NM Basic N A 100 CONN PIN REFERENCENAME _ PINFUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND_DISC_13 Reference Display Select Discrete 2 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 lt not gt Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 When there is a Terrain Alert and the FDS 255 2000 is not currently displaying Terrain it will set its range to 10 NM and Pop Up to Terrain mode The range does not change if Terrain mode is already selected when there is Terrain Alert 3 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGP WS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 230 Honeywell M
157. 6 1 243 Honeywell EDZ802 EDZ603 EDZ803 non Integrated with MK VIII Only dual SCI range Display Configuration Group 238 Display Type 7 Honeywell Non Integrated EDZ802 EDZ603 EDZ803 77 Sweep Type S Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Peaks Mode 5 3 7 Elevations via overlay Manual select ________ Anytime except when display isin or Sector Scan mode Manual deselect Anyime O Auto Range No i G Yes a magenta underline will be alternately placed and removed under the Peaks Elevations Yes for Peaks Elevations located near the vertical center on the right edge F of the Terrain image Honeywell picture bus ae 453 1 B J1 59 gi a DRE 453 2 B J1 57 1 2 Display Input Control Group 249 CHANNEL CONNECT TO SCI Bus 1 Fault Designation DISPLAY BUS 1 429 422RX 1 Format RS 422 12 0K baud Bus Tvpe Basic J2 36 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms 2 37 Range Mode Range word 6 5 1 1 80 4 discrete 2000NM Basic N A 100 Status 6 5 1 2 FF Discrete N A Basic N A 100 CHANNEL CONNECT TO SCI Bus 2 Fault Designation DISPLAY BUS 2 429RX 3 Format RS 422 12 0K baud Bus Tvpe Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 11 Range Mode Range word 6 5 1 1 80 4 di
158. 60 4314 150 REV SHEET 208 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 10 Honeywell Bendix EFIS 40 50 Integrated Display Configuration Group 8 Function Value Reference section Display Type Bendix EFIS 40 50 Integrated gc Sweep Type Sweep range 90 degrees Auto Pop Up 2 Category 7 Options Select Group 1 Peaks Mode 5 3 7 Peaks Always Enabled See Note 1 Manual select Anytime U U U Manual deselect U U U Auto Range YelONM 1 Moving Marker Overlay Page No the display supplies mode annunciation Display bus type ARINC 455 k ia 453TX_1 B J1 59 72 ppm ii 453 2 B J1 57 72 Display Input Control Group 2 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM Basic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM B
159. 7 GPS Antenna 29dB 1 EA Sensor Systems 567 1575 52 567 GPS Antenna 26dB 1 EA Sensor Systems 567 1575 133 567 GPS Antenna 33dB 1 EA Thermax M17 128 RG400 Coax Cable RG400 U EA Coax Cable RG 142B U EA PIC 14293 Coax Cable AIR EA PIC 544191 Coax Cable AIR EA ECS 311901 Coax Cable AIR EA ECS 311601 Coax Cable AR EA ECS 311201 Coax Cable EA Amp 225554 6 TNC Angle Plug Male 1 EA 440 1239 001 Amphenol 79075 TNC Angle Plug Male 1 EA 440 1239 001 NOTE Ifa satellite communication system is installed in the aircraft or the GPS cable run is in the vicinity of a VHF transceiver and or cable DO NOT USE R G 142 or R G 400 cable 1 9 3 Circuit Breaker The Circuit Breaker needs to be a 3 Amp delayed action circuit breaker Vendor Name Vendor P N Description QTY UM Klixon 7277 2 3 3 Amp Circuit Breaker 1 EA EGPWS power 28 Klixon 1 7277 2 1 1 Amp Circuit Breaker lamp 1 EA power 28 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 21 Honeywell MK VI MK VIII EGPWS Installation Design Guide 1 9 4 Annunciators amp Switch Annunciators The devices shown below are West Coast Specialties and Staco switch annunciators and are representative of those used in some installations However there are other comparable devices on the market that may be substituted at the installer customers choice The installer customer is cautioned to
160. 8 AIRCRAFT 28VDC AMP Power Input 28VDC KRA 405 Adjustable Trip Landing Gear Discrete KRA 405B Adjustable On Ground DC Gnd Trip pins W V amp F The Honeywell KRA 405B provides 3 programmable Adjustable Trip outputs that can be used to supply a ground to the Landing Gear input discrete when the aircraft is less than 5 to 20 feet Radio Altitude See the Honeywell KRA 405B Installation Manual 006 10536 0003 for details of the Adjustable Trip output Use of Adjustable Trip outputs of the KRA 405B requires CM2000 Configuration Module along with KPA900 Configuration Module Programmer PC and software The Collins ALT 55 622 2855 001 only also provides 4 shop adjustable Trip outputs pins 41 43 46 and 48 contact Collins Avionics for details FIXED LANDING GEAR FLOAT AIRCRAFT MK VI EGPWS ALTERNATE AIR SWITCH ARRANGEMENT COMPUTER Example Shown Twin Otter Not LANDING FULL LANDING FLAP POSITION 16 18 M Landing Flap Discrete LANDING SM FLAPS UP APPROACH FLAP POSITION 5 7 Landing Gear Discrete 28 AIRCRAFT 28VDC Power Input 28VDC Landing Gear Discrete On Ground DC Gnd OPTIONAL EQUIPMENT EXISTING ON AIRCRAFT HOUR METER AIR SWITCH 2 RELAY AIR STREAM NO AIR SWITCH 240 KNOTS SHOWN AS GROUND Some aircraft ex Twin Otter have an air switch flapper on the wing that can be used to provide a Landing Gear discrete gro
161. 8 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 2 6 1 GPS RS 232 Digital Serial Bus serial port 3 One port is provided for use with external or internal RS 232 GPS interfaces This port is common with the GPS RS 422 port described in Section 4 2 6 2 and can only function as a RS 232 interface or a RS 422 interface but not both Pin Assignment Signal Mnemonic Transmit J2 45 GPS TXA Receive J2 29 GPS RXA Common J2 28 GND NOTE internal GPS configuration is used 965 1190 0XX or 965 1220 0XX then the receive input will be non functional 4 2 6 2 GPS RS 422 Digital Serial Bus serial port 3 One port is provided for use with external GPS interfaces This port is common with the GPS RS 232 port described in Section 4 2 6 1 and can only function as a RS 232 interface or a RS 422 interface but not both Pin Assignment Signal Mnemonic Transmit A leg J2 45 GPS TXA Transmit B leg J2 46 GPS TXB Receive A leg J2 29 GPS RXA Receive B leg J2 12 GPS RXB NOTE If an internal GPS configuration is used 965 1190 0XX or 965 1220 0XX then the receive input will be non functional 4 2 6 3 Air Data RS 232 Digital Serial Bus serial port 2 One port is provided for use with Air Data computer or Static Pressure Sensor interfaces This port is common with the Air Data RS 422 port described in Section 4 2 6 4 and can only function as a RS 232 interface or a RS 422 interface but not both Pin Assignment Signal
162. 9 Aircraft Operator Installer Contact Contact Phone Aircraft Type be specific Engine Type model number CURRENT GPWS INSTALLATION If GPWS is currently installed in the aircraft please provide the following information COCKPIT DISPLAYS Please provide the following information for intended EGPWS display purposes include any new displays planned SYSTEM MODEL NO PART NO SOFTWARE NO EFIS Symbol Generator EFIS Display EFIS Display Control Panel Multifunction Display MFD Weather Radar Indicator Weather Radar R T Weather Radar Controller Other specify Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 139 Honeywell MK VI MK VIII EGPWS Installation Design Guide AIRCRAFT SYSTEMS INFORMATION Use if Not Applicable Please provide the manufacturer model number part number software part number quantity per aircraft and output data information for OUTPUT DATA FORMAT NOTES SYSTEM 5 MODEL PART S W PART ARINC 429 547 552 575 DC synchro potentiometer discrete etc Identify available ARINC 429 labels Air Data Computers Radio Altimeters Eel _ ee __________________ Receivers AHRS IRU GPS Altitude Reference WGS 84 _ MSL DISCRETE INPUTS Please check applicable boxes for both up and down C et PARAMETER 428VDC J MDC Flaps Down landing configurat
163. 9 LVO 208 208 95 82 SI3371 OGA 82 SI3371 208 0072002 Nd A8 jenas NI 519 Ha geq jeues HOLIVH3N3O9 TO8INAS 1331 0208 95 geq jeues H3TIOHINOO AW1dSI 1391 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 85 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide 908 88 107 Nd 908 88ZEL0Z Nd A8C 82 5144 4 82 5148 17 7 Ver sng Ionuoo A etes rn t est s 9143 14614 cas ER EAS Ieues epey D pias sng A ee sng sng f r P YOY einig YO gate NISN ES 02 800 M yy Oe WS T XM 0s9 nA WX ger geq jenas geq jeues epey NI SN 39131 LE 1 06 jenas 199138 199138 LY 11 YOLVYANAD Toss 1253938 YOLVYANAD TOSWAS LHOIY els e JO8WAS 1431 908 9S dOd 908 95 NIVYMALL c snd 5 AV 1dSIG M 020 21 596 SMd93 IIIA MIN
164. 951 0386 001 1 8 Installation Kits and Accessories NOTE Not all installation kits are immediately available contact Honeywell Order Administration 425 885 8719 for availability 1 8 1 MK VI MK VIII EGPWS Installation Kits Note For all parts in the Installation kits the weight of each part is less than 0 25 pounds A Retrofit classic MK VI GPWS installation The MK VI MK VIII EGPWS Installation Kit P N 755 7013 011 contains the following parts Vendor Name Vendor P N Description QTY UM Honeywell P N Positronic Ind RD50F10JVLC 15 P2 connector 1 EA 440 1233 001 Honeywell 700 1710 020 Configuration Module 1 EA 1700 1710 020 B New EGPWS installation The MK VI MK VIII EGPWS Installation Kit P N 755 7013 010 contains the following parts Vendor Name Vendor P N Description QTY UM _ Honeywell P N Positronic Ind DD78F10JVLC 15 P1 connector female 1 EA 440 1158 009 Positronic Ind RD50F10JVLC 15 P2 connector female 1 EA 440 1233 001 Honeywell 700 1710 020 Configuration Module 1 EA 700 1710 020 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 19 Honeywell MK VI MK VIII EGPWS Installation Design Guide Bendix King 071 04003 0002 Computer Mounting Tray 1 EA X 405 0383 001 1 8 2 RS 232 Cable The MK VI MK VIII EGPWS RS 232 Cable can be ordered using the following part numbers NOTE The RS 232 Cable can be built by the Installer Operator per the des
165. 96 Knots Approx LSB 0 125 Knots East Data 278 Complement Bina 6 2 55 Discrete Word 017 KMD 550 850 Source KMD 550 850 display LABEL Octal 017 Units N A Max Range N A Approx LSB N A Data Bits 11 Sign Bit Pad Bits N A Transmit Interval mSec 200 Data Type Discrete SDI Bits 9 10 11 16 Spares 23 Flap Override Momentary 24 29 6 2 56 Inertial Vertical Speed 365 Inertial Vertical Speed Source ARINC 704 IRS AHRS LABEL Octal 365 Units Max Range 32768 FPM Approx LSB 1 Data Bits 14 to 28 15 Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 20 to 40 Data 2 s Complement Binar SDI Bits 9 10 6 2 57 Inertial Altitude 361 6 2 58 Vertical Velocity 165 GPS Vertical Velocity GPS Source ARINC 743A GPSSU LABEL Octal 165 Units FPM Max Range 32 768 FPM Approx LSB 1 FPM Data Bits 14 to 28 15 Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 1000 Maximum Data 2 s Complement Binary SDI Bits 9 10 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 291 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 2 59 Latitude Fine 120 GPS Latitude Fine GPS Source ARINC 743 A GPSSU LABEL Octal 120 Max Range 0 000172 Deg Approx LSB 8 38 Deg Data Bits 18 to 28 11 Sign 29 Pad
166. ARINC 429 Bus 1 75 LB 8 C Bk Pa p 23 ARNG 423 M ARINC 429 Bus 2 GPS Bus LB 6 WwW uw B 0 ARINC429 DuaIGPS vsd Cat 3 429 GPS Alt ARINC Bus 1 Bus 2 Aircraft Model ID Speed Ref 743 43A A B A B 253 BD 100 255 High MSL 743A A25BP1 6A_ A25BP1 6B_ A24BP1 6A 24 1 6 CJ1 CJ2 255 High MSL 743A TBD TBD TBD TBD NOTE The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation 1 10 253 is a optional configuration for compatibility with IOC that are missing North South East West Velocities labels 3 5 7 Instructions Using Appendix E Tables 5 2 5 3 3 and 5 3 3 x as described above select the Position Input Type that matches the aircraft Position Input configuration feature preferences and version part number being installed Record the ID number for the Position Input Type from Appendix E Table 5 3 3 under the Ident No heading for Step Category 3 in Appendix E Table 5 2 Using the Position Input Type number from Appendix E Table 5 3 3 as go the Position Input Select x Table The electrical interfaces pin outs for the Position Input Select are shown in Appendix E Table 5 3 3 and are used to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 431
167. Alt 6 2 1 131 072 FT Basic 31 3 62 5 Corrected Baro Alt 6 2 38 E131 072 Basic d 31 3 62 5 Computed Airspeed 6 2 39 1024 KTS Basic 62 5 125 Barometric Rate 6 2 3 E32678 FPM Basic 31 3 62 5 Static Air Temperature 6 2 2 512 Degrees Basic 250 500 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 182 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 6 AIR DATA INPUT SELECT 6 CHANNEL CONNECT TO ADC 1 Fault Designation AIR DATA BUS 429RX 2 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Uncorrected Baro Alt 6 2 1 17 131 072 FT Basic 1 0 31 3 62 5 Computed Airspeed 6 2 39 1024 KTS Basic 0 0625 62 5 125 Static Air Temperature 6 2 2 512 Degrees Basic 0 25 250 500 Derive Baro Altitude Rate Digital Baro Altitude Rate is derived using Uncorrected Barometric Altitude Baro Rate is not available with this air data source TABLE 5 3 2 10 AIR DATA INPUT SELECT 10 CHANNEL CONNECT TO ADC 1 Fault Designation AIR DATA BUS 429RX 2 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Uncorrected Baro Alt 6 2 1 17 131 072 FT Basic 1 0 31 3 62 5 Corrected Baro Alt 6 2 38 131 072 FT Basic 1 0 31 3 62 5 Computed Airspeed 6 2 39 1024 KTS Basic 0 0625 62 5 125 Barometric Rate 6 2 3 32678 F
168. Altitude ADS 65 RT 221 300 Radio Altimeter Pitch Synchro Attitude 3 Wire Synchro 11 8 VAC Uncorrected Barometric Altitude CIC 02702 ARINC 547 578 4 Low Level Glideslope Deviation Validity Roll Attitude 3 Wire Synchro 11 8 VAC with Validity Uncorrected Barometric Altitude AZ 241 AZ 800 ARINC 547 Localizer Deviation with Discrete Valid 62 DIGITAL INPUT DATA ARINC 429 6 2 1 6 2 2 6 2 9 Uncorrected Barometric Altitude 203 Static Air Temperature 213 Barometric Altitude Rate 212 Altitude 076 GPS MSL Horizontal Integrity Limit 130 GPS Ground Speed 112 GPS Latitude 110 GPS Longitude 111 GPS Track Angle 103 GPS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV 172 173 173 173 173 174 174 174 177 177 179 187 193 194 198 241 244 248 252 255 257 258 269 269 269 269 270 270 270 270 271 271 271 272 272 272 273 273 273 274 274 275 275 275 276 276 278 278 278 278 278 278 279 279 279 SHEET 155 6 2 10 6 2 11 6 2 12 6 2 13 6 2 14 6 2 15 6 2 16 6 2 17 6 2 18 6 2 19 6 2 20 6 2 20 1 6 2 21 6 2 22 6 2 23 6 2 24 6 2 25 6 2 26 6 2 27 6 2 28 6 2 29 6 2 30 6 2 31 6 2 32 6 2 33 6 2 34 6 2 35 6 2 36 6 2 37 6 2 38 6 2 39 6 2 40 6 2 41 6 2 42 6 2 43 6 2 44 6 2 45 6 2 46 6 2 47 6 2 48 6 2 49 6 2 50 6 2 51 6 2 52 6 2 53 6 2 54 6 2 55 6 2 56 6
169. Altitude Valid is standard 28 volt discrete Total Air Temperature is from a dedicated EGPWS 500 ohm probe using 5 volt excitation from the MK VI MK VIII EGPWC Air Data Types 11 and 12 AZ 241 AZ 242 AZ 800 AZ 810 or equivalent uses Uncorrected Barometric Altitude input scaled from 3750 feet 0 volts to 50 000 feet 10 75 volts see Appendix E section 6 1 16 Baro Altitude Rate and Computed Airspeed are not required Baro Altitude Valid is standard 28 volt discrete ID 11 requires a dedicated EGPWS 500 ohm Total Air Temperature probe using 5 volt excitation from the MK VI MK VIII EGPWC ID 12 is configured without a connection to outside air temperature with temperature set not available As a result when using ID 12 the EGPWS calculation of Geometric Altitude will be less accurate than using ID 11 NOTE The analog air data interface for the MK VI MK VIII EGPWS uses a dedicated 500 ohm temperature probe This may be an unused element in a dual element probe but must not be paralleled with any other system The EGPWS provides the 5 volt excitation for the element Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 57 Honeywell MK VI MK VIII EGPWS Installation Design Guide EGPWS MK VI MK VIII Jl Analog Air Data Computer Uncorrected Altitude Out Barometric Altitude Signal Common Baro Altitude Valid 28V BIT Out 5V Excitatio
170. Angle 6 1 16 Uncorrected Barometric Altitude AZ 241 AZ 800 Data Item Signal Name AIC Algorithm Signal Dynamic Range Signal Reasonable Range Signal Open Wire Threshold Reference Dynamic Range Reference Reasonable Range Scale Input Signal Connection AIC Name Input Reference Connection External Validity Flag Connection A Ititude Feet 5000 Feet VDC Volts 3750 0 2 mVdc foot 0 75 Vdc 0 feet Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV Input Signal Connection X 1 1 21 2 J1 2 1 62 11 43 SHEET 275 Honeywell MK VI MK VIII EGPWS Installation Design Guide AIC LSB AIC Status Mask 0000200F External Validity Type Discrete Validity 28V 6 1 17 ARINC 547 Localizer Deviation with Discrete Valid Scale Loc Deviation Dots 13 333333 Dots VDC Volts pe Positive Fly Right 75 mV per DOT 0 Volts 0 DOT 11 30 fly right C 10 fly left Input Reference Connection 6 2 Digital Input Data ARINC 429 The MK VI VIII EGPWC supports 8 ARINC 429 digital receivers used to monitor broadcast data from other LRUs and to support interactive protocols Each receiver channel follows the characteristics of reference document Digital Information Transfer System DITS ARINC Characteristic 429 Transmission System Interconnect Each 429 receiver shall be connected to an
171. Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 37 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 B J2 36 Decision Height format 1 6 2 41 370 16 8192 FT Basic 0 125 100 200 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 41 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 172 40 Decision Height format 1 6 2 41 370 16 8192 FT Basic 0 125 100 200 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 247 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 9 Category 9 Navigation Input Select The following table provides identification of the Navigation type The entry in the Navigation Type corresponds to a table that provides detailed information on the configuration For example the details for Navigation Type 1 are found in Table 5 3 9 1 In this category only the following signals are defined Glideslope source selection Localizer source selection PFD Mode Select Word Selected Course Note Numerous but not all Envelope Modulation cases require a localizer input Therefore a NAV ID that supplies both Glideslope and Localizer should be selected in this category if possible However due to hardware limitations use of Localizer for installa
172. Basic Fault Designation STATIC AIR TEMPERATURE FAULT Probe element Excitation 5 1 25 J1 AA 5 V Ref Temp Input J1 63 4 42 K Ohms probe element J1 44 JT Temp In Chassis Gnd Ground GND J1 53 OAT PROBE ELEMENT Note Nominal 500 Q Temperature Probe only Resistance 0 C 5000 0 60 Connection example CIC Temperature Sensor P N 05257 2 wire Connect positive lead to both J1 25 and J1 63 Connect negative lead to both J1 44 and J1 53 Chassis Ground Other probes may have three contacts Computed Airspeed Substitute Ground Speed for Airspeed airspeed is not available with this air data input CHANNEL PIN FUNCTION CONNECTION PIN TYPE DESIGNATION Polarity Configuration References REFERENCE Barometric Altitude J1 9 Input 28V DISC 08 gt 17V Valid 6 6 22 Validity Discrete 28V lt 4 4V Invalid 4 2 7 Derive Baro Altitude Rate Analog Baro Altitude Rate is derived using Uncorrected Barometric Altitude Baro Rate is not available with this air data source Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 181 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 4 AIR DATA INPUT SELECT 4 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format DC with Validity Flag Uncorrected Barometric J1 62 6113 Input Type Basic Altitude gt 11 43 E Fault Designation BAROMETRIC ALTITUDE FAULT Va
173. C_xx 4 2 8 Configuration Module Interface System configuration is defined via a Configuration Module which resides in the MK VI VIII EGPWS aircraft wiring harness backshell The EGPWS Configuration Module contains the aircraft interface and functionality definitions specific to the installed aircraft Refer to Section 5 for interface and functional definitions by category Note that both configuration module part numbers 700 1710 003 and 700 1710 020 have identical electrical interfaces Electrical Characteristics Refer to the EGPWS Configuration Module specification Data definition Refer to the EGPWS Configuration Module specification Pin Assignment Signal Mnemonic Clock J2 32 RED SPICLK Master Data Out J2 50 BLK SPIMOSI Master Data In J2 33 ORN SPIMISO Configuration Module Select J2 49 WHT SPISEL Configuration Module 5 VDC J2 17 VIO SC PWR Configuration Module SVDC Return J2 16 BLU GND Output to Config Module Logic Low nominal Logic High nominal Clock Out Master Data Out Config Module Select INTERFACE OF EGPWS OUTPUTS TO CONFIGURATION MODULE 4 2 9 GPS Antenna Input A GPS input connector is available on the front of the MK VI EGPWS 965 1190 0XX only and MK VIII EGPWS 965 1220 0XX only Quantity 1 Cable Length Allowed Signal Loss Not more than 8 dB at 1575 42 MHz for cable and connector loss from antenna to unit Proprietary notice on title page a
174. Category 7 TA amp D Alternate Pop Up ALTERNATE POP UP SELECTED Category 7 Obstacle Awareness Enabled OBSTACLE AWARENESS ENABLED Category 7 Peaks Mode Enabled PEAKS MODE ENABLED Category 7 WGS84 Reference Selected GPS ALTITUDE REFERENCE WGS 84 SELECTED Category 7 MSL Reference Selected GPS ALTITUDE REFERENCE MSL SELECTED Category 7 Steep Approach Enabled STEEP APPROACH ENABLED activated Steep Approach Discrete 2 input discrete activated Category 7 Steep Approach Enabled AND Momentary Steep STEEP APPROACH ACTIVATED Approach switch configured and Steep Approach latch activated Glideslope Inhibit input discrete activated GLIDESLOPE INHIBITED Mode 6 Volume Control Discrete Selected MODE 6 LOW VOLUME SELECTED GND Audio Suppress Inhibit All Modes Inhibit Discrete EXTERNAL EGPWS INHIBITED Selected OR 28 V Audio Suppress Inhibit All Modes Inhibit Note Will only occur for present status as this condition Discrete Selected inhibits self tests Terrain Awareness amp TCF Inhibit input discrete activated TERRAIN AWARENESS AND TCF DISABLED GPWS Inhibit input discrete activated GPWS INHIBITED Note Will only occur for present status as this condition inhibits self tests Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 317 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 5 1 System Status Messages System Status Messages provide additional i
175. D therefore the range to use depends on the value of label 275 bit 17 5 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 6 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGPWS Self Test 7 Atthe time of this printing this configuration is not supported by Primus 1000 hardware prior to installation contact Honeywell EGPWS group for applicability Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 220 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 238 Honeywell Primus 1000 with binary Peaks Elevations MK VIII Only Display Configuration Group 243 Display Type 7 Honeywell Primus 1000 with binary Peaks Elevations Sweep Type Honeywell 47G1 y O Peaks Mode Category 7 Options Select Group 71 5 3 7 Manual select Selection is controlled by display Deselection is controlled by display Y Yes Data passed by ARINC 429 Labels 011 and 012 Yes 10 Auto Pop Up Category 7 Options Select Group 1 5 3 7 Moving Marker Yes Honeywell type Overlay Page Yes for Peaks Elevations only located middle right side of display Display bus type Honeywell picture bus
176. DATA INPUT SELECT 0 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format DC with Validity Flag Uncorrected Barometric J1 62 Input Type Basic Altitude 2 11 43 Fault Designation BAROMETRIC ALTITUDE FAULT Validity Barometric Alt Valid 28V Outside Air Temp ol Format DC Total Air Temperature 233 Input Type Basic Fault Designation STATIC AIR TEMPERATURE FAULT Probe element Excitation 5 V J1 25 2 J1 25 5 V Ref Temp Input 11 63 4 42 K Ohms probe element 1 44 63 sp Temp In 44 53 Chassis Gnd Ground GND J1 53 OAT PROBE ELEMENT Note Nominal 500 Q Temperature Probe only Resistance 0 C 5000 0 60 Connection example CIC Temperature Sensor P N 05257 2 wire Connect positive lead to both J1 25 and J1 63 Connect negative lead to both J1 44 and J1 53 Chassis Ground Other probes may have three contacts e Airspeed No b s BE Substitute Ground Speed for Airspeed airspeed is not available with this air data input CHANNEL PIN FUNCTION CONNECTION PIN TYPE DESIGNATION Polarity Configuration References REFERENCE Barometric Altitude EL 28V DISC 08 gt 17V Valid NE E 6 22 Validity Discrete 28V lt 4 4V Invalid NE E 2 7 Configuration Data Type Summary Data Derive Baro Altitude Rate Analog Baro Altitude Rate is derived using Uncorrected Barometric Altitude Baro Rate is not available with this air data source TABLE 5 3 2 1 AIR
177. DATA INPUT SELECT 1 CHANNEL CONNECT TO ADC 1 Fault Designation AIR DATA BUS 429RX 2 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Uncorrected Baro Alt 6 2 1 17 131 072 Basic 1 0 31 3 62 5 Computed Airspeed 6 2 39 14 1024 KTS Basic 0 0625 62 5 125 Barometric Rate 6 2 3 11 32768 FPM Basic 16 0 31 3 62 5 Static Air Temperature 6 2 2 11 512 Degrees 0 25 250 500 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 180 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 2 AIR DATA INPUT SELECT 2 CHANNEL CONNECT TO ADC 1 Fault Designation AIR DATA BUS 429RX 2 Format ARINC 575 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Uncorrected Baro Alt 6 3 2 Computed Airspeed 6 3 4 Barometric Rate 6 3 3 Static Air Temperature 6 3 1 131 072 FT Basic 1 0 31 3 62 5 1024 KTS Basic 0 125 62 5 125 20480 FPM 10 0 31 3 62 5 512 Degrees Basic 0 5 250 500 TABLE 5 3 2 3 AIR DATA INPUT SELECT 3 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format DC with Validity Flag Uncorrected Barometric J1 62 6110 Input Type Basic Altitude 1 43 m Fault Designation BAROMETRIC ALTITUDE FAULT Validity Barometric Alt Valid 28V Outside Air Temp Format DC Total Air Temperature Input Type
178. DE 97896 DWG NO 060 4314 150 REV SHEET 55 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 3 7 Runway Length MK VIII EGPWS only Two minimum runway length options are defined for Bizjet Turbofan aircraft A 2000 ft minimum runway length or a 3500 ft minimum runway length may be chosen based on aircraft type as is identified in Appendix E Table 5 3 1 This option does not effect the mode curves as discussed above and it is only available on MK VIII EGPWS 3 3 8 Instructions Using Appendix E Tables 5 2 and 5 3 1 as described above select the Aircraft Mode Type that matches the aircraft configuration feature preferences and version part number being installed Step 1 Is the aircraft a turbofan YES goto Step 2 NO goto Step 3 NO use ID 254 NO goto Step 5 Step 4 200 170 150 Flap alert preferred 200 use ID 2 170 use ID 0 150 use ID 1 Step 5 170 150 Flap alert preferred 170 use ID 3 150 use ID 4 Record the ID number for the Aircraft Mode Type from Appendix E Table 5 3 1 under the Ident No heading for Step Category 1 in Appendix E Table 5 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 56 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 4 Category 2 Air Data Input Select Category 2 defines the Air Data interface The Air Data input currently defines 4 analog and 6 digital air da
179. Disable configuration NOT selected 3 TCF INOP Precond itions a TCF Disable configuration NOT selected TRUE causes TCF INOP 4 TAD INOP Preconditions a TAD TCF Inhibit Discrete NOT selected and b TAD Disable configuration NOT selected 5 Windshear INOP Precondition The windshear algorithm has been defined within the current aircraft configuration Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 318 8 8 Honeywell MK VI MK VIII EGPWS Installation Design Guide CONNECTOR INTERFACE 1 Pinout for Front Connectors sorted by pin number Table 8 1 1 Pin Assignment For Front Connectors Sorted by Pin Number Connector Hans Pin Designation Signal Usage Summary Reference J1 09 28V DISC 08 Barometric Altitude Validity Discrete 28VDC J1 10 GS VAL L Glideslope Deviation Low Level Validity or a ies Localizer Deviation left J1 11 28V DISC 06 Glideslope Validity Discrete 28VDC J1 12 GND DISC 09 Terrain Awareness and TCF Inhibit Discrete Ground J1 14 GND DISC 07 Flap Override Discrete Ground J1 13 GND DISC 08 Mode 6 Low Volume Discrete Ground i 31 226 Oef J1 27 922 Radio Altitude Validity Discrete 28VDC Glideslope Deviation Low Level Validity or ios Localizer Deviation right I i 5 S Spare Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SI
180. Discrete 2000NM Basic N A 100 CHANNEL CONNECT TO Fault Designation 429RX 3 Bus Type q NoConmecon _________ CONN REFERENCE NAME PIN FUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429 1 Low Speed J2 43 B J2 42 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x Integration Notes 1 Radar Indicator part number must end in X1X 2 This display type overlays an inverted T aircraft symbol Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 214 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 18 KC Picture Bus without presentation of Geometric Altitude Display Configuration Group 17 Display Type KC PictureBus KCPBY 0 O Sweep Type Curtain Vertical orHorizontalscan Auto Pop Up 53 Peaks Mode Category 7 Options Select Group 71 5 3 7 Elevations via overlay Manual select _________ None Display controls selection y O Manual deselect None Display controls selection Auto Range Controlled by display response if selected 10 NM range willbeused Moving Marker Overlay Page Controlled by display Display bus type KCPB 52377 24 453TX_1 B
181. E CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 287 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 2 43 Longitudinal Acceleration 331 LONGITUDINAL ACCELERATION Source IOC LABEL Octal 331 Max Range 4 0 g s Approx LSB 0 000977 g s Data Bits 17 to 28 12 Sign Bit 29 Pad Bits 11 to 16 Transmit Interval mSec 10 to 20 Data Type 2 s Complement Binar SDI Bits 9 10 6 2 44 Left Body Angle of Attack 224 Body Angle of Attack Source IOC LABEL Octal 224 Max Range 180 degrees Approx LSB 0 0439 degrees Data Bits 17 to 28 12 Sign 29 Pad Bits 11 to 16 Transmit Interval mSec 50 to 100 Data 278 Complement Binary SDI Bits 9 10 6 2 45 Right Body Angle of Attack 225 6 2 46 VOR ILS Frequency 034 VOR ILS Frequenc LABEL Octal 034 Data Bits See NOTE N A Sign Bit N A Pad Bits N A NOTE This input is used to indicate 1f the VOR ILS receiver 1s tuned to an ILS frequency or to a VOR frequency BIT 14 will be set to a 0 for all VOR frequencies and to a 1 for all ILS frequencies by the tuning information source 6 2 47 PFD Mode Select Word 163 PFD MODE SELECT WORD Type 4 NOTE 1 Transmit Interval for data from PFD via IOC is 250 mSec Maximum NOTE 2 BITS 25 to 28 contain Binary Code for Displayed Data Source as listed below NOTE 3 BITS 19 20 indicate MDA selection status and BIT 21 indicates DH selection status as l
182. ED EXPANSION GA FAST Turboprop 220 knots to 310 knots GA SLOW Turboprop 190 knots to 280 knots BIZJET Turbofan 220 knots to 310 knots Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 54 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 3 4 Mode 3 type Two Mode 3 alert curves are defined GA Turboprop and Bizjet Turbofan The GA Turboprop Mode 3 curve is equivalent to the classic MK VI Mode 3 curve The Bizjet Turbofan Mode 3 curve is equivalent to the MK V MK VII EGPWS Mode 3 curves 3 3 5 Mode 4 type Mode 4A Too Low Gear expanded alert transition occurs at 178 knots for GA Fast aircraft 148 knots for GA Slow aircraft and 190 knots for Bizjet aircraft Mode 4B Too Low Flaps upper boundary has four defined levels 245 ft 200 ft 170 ft and 150 ft The 245 ft boundary is added to emulate the MK V VII Mode 4B boundary The 200 ft boundary is added to emulate the MK Mode 4B boundary The 150 ft boundary Alternate Mode 4B is for those aircraft types that routinely delay full flap deployment All other aircraft types would use the 170 ft boundary Normal Mode 4B For aircraft with previously installed classic MK VI GPWS the Normal Alternate Mode 4B correspond to the Alternate Mode 4B program pin J1 25 The following table compares Mode 4 boundaries for each Boundaries Mode 4 Aircraft type M
183. EFERENCE coer sss umm cgo mem BENI TANTUM TII E o owu orws woene es _ GPWS Warning Discrete 7 4 1 J1 78 DISC_OUT_1 Output Terrain Awareness Caution or Warning 7 4 7 1 Obstacle Awareness Caution or Warning 7 4 7 2 oupa GPs Alen Discrete Gidesope Oni ue ouput Gidesape ae 0 71 Our e owu r2 ouput Terain Displey Deces 179 J1 52 DISC OUT 7 Output Steep Approach Discrete TAM os J1 48 28V DISC 11 Not Defined in this ID Note 3 O P 12 15 28V DISC 13 Not Defined in this ID Note 3 p iue J1 50 MON OUT 3 Output Not Defined in this ID Note 3 el PRESENT Configuration Data Possible States Type 1 2 1 Flashing Lamps Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word bit if configured by the display type Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG
184. EGPWS MK VI MK VIII J1 Radio Altimeter R T 64 FRA vi Analog Radio Altitude d ARINC 552 ALT 55 45 X2 I 200 300 Radio Altitude Valid 28V 29 Valid Radio Altimeter Indicator NE s wiper DH Discrete Gnd 33 c DH out 8 Analog RA vsd Vendor Model Cat Ind DH R T R T Indicator ID wiper out Valid Collins ALT 55 ALI 55 1 P1 R V P1 57 P1 59 P1 49 Honeywell HG7502 BC JG1072 0 1 4 47 P4 46 P4 27 Honeywell RT 221 300 RA 315 0 P1 F P1 X P1 N P1 Y Honeywell RT 220 300 RA 215 3 P1 F P1 N P1 W P1 Y Honeywell KRA 405 KNI 415 416 4 P1 M A P1 B P1 g P1 L Honeywell KRA 405B KNI 415 416 4 P1 M A P1 i 1 1 Honeywell ALA 51A 51 0 2 P1B 47 1 46 P1B 27 Collins 860 1 339H 1 2 0 1 P1B 47 P1B 46 P1B 27 NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation NOTE 1 The following RT 300 part numbers meet ARINC 552 for the Auxiliary Output 7001840 902 906 912 916 917 918 922 926 928 932 936 937 and 938 RT 221 s are also compatible consult your Honeywell representative NOTE 2 This is the Precision Output from the R T Note the and signals are swapped to convert the 4mV to 4mV RT 300 901 903 905 should use the Precision Output same as RT 220 3 10 5 Digit
185. EL Octal 326 Units Deg Sec Max Range 77 128 Degrees Sec Approx LSB 0 0156 Deg Sec Data Bits 16 to 28 13 Sign Bit 29 Pad Bits 11 to 15 Transmit Interval mSec 10 to 20 Data Type 2 s Complement Binary SDI Bits 9 10 6 2 50 Body Roll Rate 327 Body Roll Rate Source AHRS IOC Max Range 128 Degrees Sec 6 2 51 Minimum Descent Altitude 170 IOC Scaling Units Feet Above Sea Level ASL Note 1 Some IOC configurations may only provide positive ranges 0 to 65536 feet however the EGPWS supports both positive and negative ranges 65 536 feet for all configurations Note 2 This label may be provided in a configuration with a single DH input or in conjunction with a selected MDA input For those configurations which provide DH and MDA on separate labels format 3 applies Format 1 is 0 0 SDI Format 2 is Left SDI used and Format 3 is no SDI 6 2 52 Normal Angle of Attack 236 Normal Angle of Attack Source IOC LABEL Octal 236 Units N A Max Range 0 to 1 Approx LSB 0 000031 Data Bits 14 to 28 15 N A Sign Bit N A Pad Bits 11 to 13 29 Transmit Interval mSec 80 Data 2 s Complement Binary SDI Bits 9 10 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 290 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 2 53 North South Velocity 166 GPS Source ARINC 743 A GPSSU Units Knots Max Range 4 0
186. FG gt prompt type CMR lt Enter gt Each category and its associated ID is read from the Configuration Module and listed on the PC display Alternately when not in the Configuration sub mode the command PS lt Enter gt Present Status will display the EGPWC and Configuration Module data 7 Configuration Module reprogramming is complete 4 6 Terrain Database Loading 4 6 1 Effectivity The MK VI EGPWS 965 1180 0XX and 965 1190 0XX are shipped from the factory loaded with the Regional Terrain Database requested when the purchase order was placed Use operation of a MK VI EGPWS outside of the loaded Regional Terrain Database will result in the Terrain Awareness function being unavailable Aircraft operating outside the loaded Regional Terrain Database region will have to load one of the other two Regional Terrain Databases before beginning the ground test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 122 Honeywell MK VI MK VIII EGPWS Installation Design Guide The MK VIII EGPWS 965 1210 0XX 965 1220 0XX have a Global Terrain Database 4 6 2 Description This modification consists of loading the PCMCIA card into the EGPWS either In The Aircraft or On The Bench An optional verification procedure is provided 4 6 3 Approval This procedure contains no modification information that revises the approved configuration and therefore does not require
187. Flap Override switch Category 13 ID s 254 amp 255 do not support this function see 3 15 1 2 This feature is activated by momentarily pressing a light switch located in the cockpit within sight of each pilot When Flap Override is selected and active the EGPWS will illuminate a GPWS FLAP OVRD light J1 73 see 3 14 2 8 to remind the pilots that this feature has been activated After landing both the function and the light will automatically reset to the OFF condition The Flap Override function and light can also be manually deactivated in flight by again pressing the light switch Each pressing of the light switch during flight will alternate the ON OFF state of this function minimum of 5 seconds between presses The use of the Flap Override switch will be controlled by the Operator s Air Carrier Airline Operational Procedures Discrete Position Status Connector Pin Flap Override OVRD Toggle Gnd J1 14 Normal Open 3 15 1 7 Mode 6 Low Volume Discrete The Mode 6 Low Volume discrete permanently or temporarily modifies the volume of the Mode 6 altitude and bank angle callouts This discrete operates independent of the Category 14 options The Mode 6 Low Volume discrete is used to reduce the Mode 6 volume by 6dB from the volume level select in Category 14 This discrete is typically connected to ground to lower the volume an additional 6dB In some installations it is connected to the windshield wiper c
188. Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate J2 37 Mode Display Word 1 6 2 26 270 Discrete Mode Tilt Gain Basic N A 100 ms 2 36 Range Display Word 2 6 2 20 271 Discrete 5 320NM Basic N A 100 ms CHANNEL CONNECT TO WX IND 429 Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate J2 412 Mode Display Word 1 6 2 26 270 Discrete Mode Tilt Gain Basic N A 100 ms J2 40 Range Display Word 2 6 2 20 271 Discrete 5 320NM Basic N A 100 ms CONN PIN REFERENCE NAME PIN FUNCTION Polarity Configuration J1 32 GND DISC 12 Reference Display Select Discrete 1 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 Either Weather WX or Weather Test pattern must be displayed before Terrain can be viewed The white Weather annunciation WX will still be present when Terrain is displayed 2 When interfacing to a single display controller configuration the bus
189. GPS BUS 429RX 4 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 1000 Altitude 6 2 4 131 072 FT Basic 0 125 1000 VFOM 6 2 13 1024 meters Basic 0 125 1000 HFOM 6 2 10 1024 meters Basic 0 000061035 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125 1000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 1000 Sensor Status 6 2 16 Discrete Wd Basic n a 1000 UTC 6 2 17 Discrete Wd Basic 0 1 min 1000 Date 6 2 18 Discrete Wd Basic 1 day 1000 Notes Slowest acceptable update rate in milliseconds This label is not required Data used if present Table 5 3 3 12 Position Input Type 12 High Speed ARINC 743A GPS no N S E W Velocities CHANNEL CONNECT TO GPS ARINC 743A Fault Designation GPS BUS 429RX 4 Format ARINC 429 High Speed Bus Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 1000 Altitude 6 2 4 131 072 Basic 0 125 1000 VFOM 6 2 13 32768 ft Basic 0 125 1000 HFOM 6 2 10 16 nm Basic 0 000061035 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125
190. GPWS will record approximately 40K bytes per minute of data 1 hour of recorded time would be approximately 2 4MB most laptops have 1GB or more free space e Use the Event Marker F9 key to identify events during tests e Use the F10 key to roll increment the history file name between test sequences Rolling adds a number to the end of the filename or increments the existing number if possible Example use tail number N3GC in the file name with a file number 01 this gives a filename N3GC01 hst which will roll to N3GC02 hst when the F10 key is pressed 5 2 7 Pilots Guide Honeywell has developed a Pilot s Guide for the MK VI MK VIII EGPWS drawing number 060 4314 000 that provides a description of the modes and the controls of the EGPWS 5 2 8 Failure Modes Effects and Safety Analysis Honeywell has developed a Failure Modes Effects and Safety Analysis document for the MK VI MK VIII EGPWS drawing number 060 4199 182 that provides an analysis of the failure modes of the EGPWS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 129 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION VI MK VI GPWS classic to EGPWS MK VI VIII Pin to Pin Comparison Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 130 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION VI MK VI GPWS to
191. GURATION TYPES 5 2 CONFIGURATION SELECTION 5 3 CONFIGURATION SELECTION TABLES 5 3 1 5 3 2 5 3 3 5 3 4 5 3 5 5 3 6 5 3 7 5 3 8 5 3 9 5 3 10 5 3 11 5 3 12 5 3 13 5 3 14 5 3 15 5 3 16 5 3 17 Category 1 Aircraft Mode Select Category 2 Air Data Input Select Category 3 Position Input Select Category 4 Altitude Callouts Category 5 Audio Menu Select Category 6 Terrain Display Select Category 7 Options Select Group 1 Category 8 Radio Altitude Input Select Category 9 Navigation Input Select Category 10 Attitude Input Select Category 11 Heading Input Select Category 12 Windshear Input Select Category 13 Input Output Discrete Type Select Category 14 Audio Output Level Category 15 Undefined for this software release Category 16 Undefined for this software release Category 17 Undefined for this software release 6 CONFIGURABLE INPUT DATA DEFINITION 61 ANALOGINPUT DATA 6 1 1 6 1 2 6 1 3 6 1 4 6 1 5 6 1 6 6 1 7 6 1 8 6 1 9 6 1 10 6 1 11 6 1 12 6 1 13 6 1 14 6 1 15 6 1 16 6 1 17 ARINC 552 Radio Altimeter ALT 55 Radio Altimeter Uncorrected Barometric Altitude Outside Air Temperature 500 ohm probe Outside Air Temperature Internal Constant ARINC 547 578 4 Low Level Glideslope Deviation with Discrete Valid ARINC 547 578 4 Low Level Glideslope Deviation with Low Level Valid Roll Attitude 3 Wire Synchro 11 8 VAC Magnetic Heading 5 Wire Synchro Uncorrected Barometric
192. Ground NOTE Some PC Comm Ports have Pins 2 amp 3 reversed from what is described above The mating connector for the EGPWS J3 test connector is a male pins 15 pin double density D subminiature type Positronics Industries kit part number ODD15M1OYOZ or the following individual parts Nomenclature AMP Amp Part Number Military Part Number Peackshel Shields Clamp 2 required 440 Male Jckscron n geweses eme The following tools will work with Positronics Amp and Mil Spec Connectors Insertion Extraction Tool 91067 1 M81969 1 04 Hand Crimp Tool M22520 2 01 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 146 Honeywell MK VI MK VIII EGPWS Installation Design Guide WinVIEWS OPERATION Windows Virtual Interface to the Enhanced Warning System WinVIEWS software is a tool developed by Honeywell to monitor or view values within the EGPWS The WinVIEWS software provides a monitor function that does not alter the operation of the EGPWS The monitoring of values assists in the installation testing of the EGPWS by allowing the operator to quickly determine if the correct signal and scaling is being used by the EGPWS Additionally WinVIEWS provides a detailed status of the software configuration and input signals which enables quick identification of system anomalies The command fil
193. Group 253 CHANNEL CONNECT TO WX IND 429 Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND 429 Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B 2 40 Range 6 2 20 273 N A 5 320NM Basic N A 100 Output 429 Bus Group 0 Channel Pins Comments 429TX_1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x 2 42 Integration Notes 1 EGPWS ARINC 429 Output Bus must be connected to the display 2 When there is a Terrain Alert and the FDS 255 2000 is not currently displaying Terrain it will set its range to 10 NM and Pop Up to Terrain mode The range does not change if Terrain mode is already selected when there is a Terrain Alert 3 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 238 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 254 Collins ProLine 21 Integr
194. HANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Tvpe Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Mode Range Word 6 2 21 176 Discrete 5 640NM Basic 50 Output 429 Bus Group 1 Channel Commets 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x J2 42 429TX 2 Low Speed A J2 26 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x B J2 9 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 3 The Peaks mode will support blue water on displays that can support blue 4 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGPWS Self Test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 239 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 255 Honeywell SPZ8000 older style MK VIII Only Display Configuration Group 255 Function Reference section Display Type
195. HO9IJNOO 343 JHL SI 2 LYWYO4 Gl 3dAL 3133 9SIG AHODALVS 3HL NOILVYNSIANOD G3YINDAY SI 08 0 51 9 1 01 3dAL AVIdSIG 9 AHOO31VO IHL Suvavs YSHLVSM JHL OL 3OVAS31NI SLAIdWOO l TWNNVW SIHL dO NOILO3S NVOVH H3HIV3M OL 48384 Z dO SNA 65 IHL 304 318 0 Xvuavno 0000 79000 20 5 2000 92 21 ISN L 5310 JN NI 31382SIO 03193135 NIVHH3L ZZ vi S9rd NI 31359819 NiVHH3L 7 8 Sng 1 0 22 100 862v HSLLINSNVYL 18 LNO 62 HALLINSNVYL 89 gc 59 95 ONDI XIQN38 YOLVYANAS 1OSNAS GIN A 1noSGzpH3llWSNVHLIM 1nov6zeHSLIWSNvHl zz 9S SNDI XION3S ge HE HOIVH3N39 108WAS L 31ON 33S gt gt 3lON 33S a 1 31ON 33S 1S31 Ol SS3Hd YOLVIONNNNY AV1dSIG A AV sna YOLVIONNNNY 31v NH3 L1V NO 7 v4 SMd93 5 TWWHON LSLON 33s AD c ASAL O1 Ss3ud o gt 1 YOLVIONNNNY ss sna UII YOLYIONNNNY vs gt SOINOIAV 09 SMd93 is JION 33 336 E aS 85 1 336
196. Heading ARINC 429 via dual IOC buses Note 1 m Note 1 ID 254 255 may only be used in conjunction with other IOC bus selections for categories 2 6 8 9 10 and 12 Note 2 Category 10 and Category 11 use the same ARINC 429 receiver if a digital source is selected Table 5 3 11 0 Heading Input Select 0 SUMMARY DATA X 11 22 Format 5 Wire Synchro with Validity Flag Y 1 23 Input Basic 2 3 Fault Designation MAGNETIC HEADING FAULT Reference Validity Magnetic Heading Validity Discrete 28V A J1 4 Reference Nominal 26 VAC 11 24 REFERENCE Magnetic Heading J1 28 Input 28V_DISC_10 gt 17V Valid 6 6 23 Validity Discrete lt 4 4 Invalid 4 2 7 Table 5 3 11 2 Heading Input Select Type 2 CHANNEL CONNECT TO AHRS Fault Designation AHRS BUS 429RX 7 Format ARINC 429 High Speed Bus Tvpe Basic Magnetic Heading Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 23 Magnetic Heading 6 2 32 320 15 180 degrees Basic 0 0054931640625 10 20 B J2 6 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 255 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 11 3 Heading Input Select Type 3 CHANNEL CONNECT TO AHRS Fault Designation AHRS BUS 429RX 7 Format ARINC 429 High Speed Bus Type Basic Data Reference Label Sig Bits Range Sig
197. Honeywell Airlines amp Avionics Products Honeywell Inc 15001 N E 36th Street Redmond WA 98052 MK VI MK VIII Enhanced Ground Proximity Warning System Class A TAWS Installation Design Guide Hardware Software Part Numbers 965 1180 020 965 1190 020 965 1210 020 965 1220 020 Release Date July 14 2003 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 1 OF 326 Honeywell MK VI MK VIII EGPWS Installation Design Guide Copyright 2003 Honeywell Inc All rights reserved This document and all information and expression contained herein are the property of Honeywell International Inc and is provided to the recipient in confidence on a need to know basis Your use of this document is strictly limited to a legitimate business purpose requiring the information contained therein Your use of this document constitutes acceptance of these terms Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 2 Honeywell MK VI MK VIII EGPWS Installation Design Guide Typed names constitute approval signatures Actual signatures are on file at Honeywell in Redmond WA pe f 1122220 Dem REVISION r OF SHEETS INDEX ADDED SHEETS SHEETS SHEET NUMBER SHEET SHEET SHEET SHEET NUMBER NUMBER NUMBER NUMBER LTR LTR LTR REVISIONS DESCRIPTION DA
198. Honeywell 5x6 SPZ8000 older style does not blank every fourth weather radar display line This interface supports SG 810 and SG 811 SPZ8000 systems only Sweep Type Honeywell Auto Pop Up Category 7 Options Select Group 1 3 7 amp Alternate Pop Up False TA amp D Alternate Pop Up True Pop Up On Caution or Warning Up On Caution or E Never lu NevrPoUp Up Peaks Mode 5 3 7 Elevations via overlay Manual select 7 Selection is controlled by display Manual deselect Deselection is controlled by display Auto Range Yes IONM Moving Marker Yes Honywelltyp Yes for Peaks Elevations only located on lower right side Display bustype Honeywell picture bus LE 453 1 1 58 Terrain Display data to switching relay Symbol Generator 1 4 2 13 2 _____ DISPLAY BUS 2 CONNECT TO iii ii Z J1 56 Terrain Display data to switching relay Symbol Generator 2 4 2 13 2 Display Input Control Group 255 CHANNEL CONNECT TO SCI Bus 1 Fault Designation DISPLAY BUS 1 429 422RX 1 Format RS 422 12K baud Bus Type Basic J2 36 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 37 Range Mode Range Word 6 5 1 1 80 4 discrete 2000NM Basic N A 100 Output 429 Bus Group 0 Channel Pins Comments 429TX_1 L
199. I EGPWS Installation Design Guide 3 2 7 Audio Output The audio outputs consist of both an 8 ohm amplifier and a transformer isolated 600 ohm output Audio output messages are provided as specified in the selected Audio Menu Category 5 when inputs are valid and the audio inhibit discretes are not active When audio inhibit is enabled the output discrete s associated with suppressed message s are active 3 2 8 Discrete Outputs The MK VI MK VIII EGPWS provides for up to twelve 0 5 amp nominal 1 amp maximum Ground Open discrete outputs The discrete outputs are defined in Appendix E Section 4 2 11 and Category 13 The discrete outputs are optional if the ARINC 429 output data is used for driving the alert warning lamps via a symbol generator Most Aircraft Types do not use the ARINC 429 output data for lamp control This data is typically sent to the Flight Data Recorder All outputs to lamps are driven by solid state switches to ground These outputs can also be used as discrete drivers for other devices e g terrain display switching Output discretes are intended to operate with 28 VDC lamp sources and will not operate with 5 VDC lamp sources 3 2 9 Configuration Module The EGPWS aircraft configuration is programmed into a configuration module installed in the aircraft wiring This Configuration Module is identified as Honeywell part number 700 1710 020 The configuration module is installed as part of the P2 mating connector ba
200. INDSHEAR WINDSHEAR 6 X i MODE 4 TOO LOW TERRAIN TOOLOWTERRAIN gt 1 0 0 TCF TOO LOW TERRAIN TOOLOWTERRAIN 1 MODE 6 ALTITUDE CALLOUTS SELECTEDCALLOUTS 1 MODE4TOOLOWGEAR TOOLOWFLAPS 1 MODE 4 TOO LOW FLAPS TOOLOWFLAPS 1 MODE 5 GLIDESLOPE MODE 1 SINKRATE SINKRATE 5 Note The basic warning is SINKRATE PAUSE SINKRATE However if the Mode 1 Pullup curve is violated only a single Sinkrate may occur prior to the pull up voice MODE 3 DON T SINK DON T SINK PAUSE DON T SINK MODE 5 GLIDESLOPE GLIDESLOPE MODE 6 BANK ANGLE BANK ANGLE PAUSE BANK ANGLE BANK ANGLE BANK ANGLE Honeywell Algorithm at low altitudes MODE 7 WINDSHEAR CAUTION QUIET or CAUTION WINDSHEAR if Caution voice Enabled Note 1 These are the only voices that can interrupt Note 2 The preface voices will always be given prior to the warning voice Note 3 Voice message is continuous Note 4 Voice message will repeat every 10 seconds Note 5 Long Self Test will only issue a single Sinkrate Note 6 The Windshear Alerts will only be given on a MK VIII EGPWS with Windshear enabled per Category 12 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 197 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 6 Category 6 Terrain Display Select The following table 5 3 6 has an identification number ID
201. IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Range Signal Type Resolution Rate ms Uncorrected Baro Alt 6 2 1 17 E131 072 FT Basic 1 0 31 3 62 5 Corrected Baro Alt 6 2 38 17 131 072 FT Basic 1 0 31 3 62 5 Computed Airspeed 6 2 39 E1024 KTS Basic 0 0625 62 5 125 True Airspeed 6 2 40 2048 KTS Basic 0 0625 62 5 125 Barometric Rate 6 2 3 32678 FPM Basic 16 0 31 3 62 5 Static Air Temperature 6 2 2 512 Degrees Basic 250 500 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic Data Reference Signal Type Resolution Rate ms Uncorrected Baro Alt 6 2 1 E131 072 FT Basic 31 3 62 5 Corrected Baro Alt 6 2 38 131 072 FT Basic 31 3 62 5 Computed Airspeed 6 2 39 E1024 KTS Basic 62 5 125 True Airspeed 6 2 40 2048 KTS Basic 62 5 125 Barometric Rate 6 2 3 32678 FPM Basic 31 3 62 5 Static Air Temperature 6 2 2 512 Degrees Basic 250 500 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 186 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 3 Category 3 Position Input Select The following table provides identification of the Position source signal Each entry in the Position Input Type column has a corresponding table that provides detailed information on the configuration For example the details for Position Input Type 0 a
202. J2 05 429RX 6B LS ARINC 429 Input B leg J2 07 429RX 8B Spare ARINC 429 Input B leg i J2 08 429RX_4B GPS ARINC 429 Input B leg J2 09 429TX_2B EGPWS ARINC 429 Output 2 B leg J2 10 ADC_RXB SCI Display Range 2 RS 422 Receive leg port 2 ___________ 1 67 GND DISC 14 GPWS Inhibit Discrete Ground 243 _ 42TXGPSB J244 GND Configuration Module Power 5VDC Configurable Synchro 1 Z leg Radio Altitude ARINC 429 Input A leg Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 320 Honeywell MK VI MK VIII EGPWS Installation Design Guide Channel Connector 6 2 Designation Signal Usage Summary Reference GPS 2 ARINC 429 Input A leg RS 422 Transmit A leg port 2 GPS RS 232 Common port 2 amp 3 J2 29 GPS_RXA GPS RS 232 Receive port 3 50 429TX GPS A J2 34 26REF_2H 26VAC Reference 2 H J2 35 26REF 2L 26VAC Reference 2 L J2 36 429 422RX_1B Display Range 1 ARINC 429 Input B leg SCI Display Range 1 RS 422 Input A leg port 1 IOC 1 ARINC 429 Input B leg J2 37 429 422RX 1A Display Range 1 ARINC 429 Input A leg SCI Display Range 1 RS 422 Input B leg port 1 IOC 1 ARINC 429 Input A leg J2 38 429RX 2B Air Data ARINC 429 Input B leg J2 39 429RX 2A Air Data ARINC 429 Input A leg J2 40 Display Range 2 ARINC 429 Input B leg 256 IOC 2 ARINC 429 Input B leg J2 41 Display Range 2 ARINC 429 In
203. K VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 248 Honeywell Primus 1000 MK VIII Only Display Configuration Group 248 Display Type Honeywell Primus 1000 j Sweep Type Honeywell ZJ Peaks Mode Category 7 Options Select Group 71 5 3 7 Deselection is controlled by display Auto Range Yes 1ONM Moving Marker Yes Honeywell type Overlay Page Yes for Peaks Elevations only located middle right side of the display Display bus type Honeywell picture bus DISPLAY BUS 1 amp 2 CONNECT TO 453TX 1 A J1 58 Terrain Display data to switching relay Symbol Generator B J1 59 CONNECT TO Not supported for this display type Display Input Control Group 248 CHANNEL CONNECT TO IC600 1 FDR Bus Fault Designation FDR BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Tvpe Basic Auto Pop Up Category 7 Options Select Group 71 5 3 7 A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 36 Range 6 2 23 050 Bits 11 14 2000NM Basic N A 100 Discrete Word 6 2 28 275 Bit 17 Discrete Basic N A 500 CHANNEL CONNECT 600 2 FDR Bus Fault Designation FDR BUS 2 429RX 3 Format ARINC 429 High Speed Bus Type Basic J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range 6 2 23 050 Bits 11 14 2000NM Basic N A 100 Discrete Word 6 2 28 275 Bit 17 Discrete Basic N A 500 Output 4
204. MK VI VIII EGPWS Signal Mapping Connector Pin Out Sorted By Pin Number USE FOR REFERENCE ONLY shaded area indicates function change X Indicates same function Signal Name GPWS 965 0686 001 020 Signal Type lt Q Signal Name MK VI MK VIII EGPWS Enhanced Roll Attitude Synchro X Roll Attitude Synchro X Chassis Ground J102 lt ACAnalog3w3 Roll Attitude Synchro Z Spare 1 Program Pin ProgPin __ 1 03 lt ACAnalog3w1 Magnetic Heading Synchro Z Alternate Airspeed Expansion Program Pin ProgPin 04544 lt ACAnalog H 26 VAC Reference 1 H Fixed Landing Gear Program Pin ProgPin __ 1 05 lt ACAnalog3w1 Pitch Synchro X Audio Volume Control 2 Program Pin 2496 ACAnalog3W3 Pitch Synchro 2 i a x 200 Altitude Callout Program Pin J1 07 lt AC Analog3W2 Pitch Synchro Y Radio Altimeter ALT 55 Scale Program Pin J1 08 Autopilot Engaged Discrete 28VDC Barometric Altitude Rate Validity 28VDC Discrete X J1 09 Barometric Altitude Validity 28VDC Glideslope Deviation Low Level Validity L 22 and Glideslope Deviation Validity 28VDC Discrete X ji lt 28vDisc Glideslope Deviation Validity 28VDC Spare Reserved X 3112 lt GDisc Terrain Awareness amp TCF Inhibit Discrete GND Altitude Callouts Volume Reduction Discrete GND X 4 133 lt GDisc Mode 6 Low Volume Discrete GND GPWS Flap Override Di
205. MK VIII EGPWS Installation Design Guide 3 4 4 Shadin 2000 Cat 2 ID 10 Air Data Type 10 Shadin 2000 or equivalent is a low speed digital ARINC 429 signal having the air data labels 203 204 206 and 212 Total Air Temperature is from a dedicated EGPWS 500 ohm probe using 5 volt excitation from the MK VI MK VIII EGPWC EGPWS MK VI MK VIII ARINC 429 Air Data A A ARINC 429 Bus Hi ARINC 429 Low Speed Air Data Bus B B ARINC 429 Bus Lo 5V Excitation 500 ohm Temp Input Temperature Chassis Ground Shadin2000 vsd Cat 2 Bus 1 Bus 2 Vendor PN ID A B A B 962830 1 2 3 10 42 7 42 8 962830 1 2 3 41 40 1 22 962830A X S 4 10 962830A X S 5 NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 61 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 4 5 Digital ARINC 429 Dual IOC Buses Cat 2 ID 255 Air Data Type 255 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having the air data labels 203 204 206 210 212 and 213 ID 255 may only be used in conjunction with other IOC bus selections for categories 6 8 9 10 11 and 12
206. Mnemonic Transmit J2 27 ADC TXA Receive J2 11 ADC RXA Common J2 28 GND 4 2 6 4 Air Data RS 422 Digital Serial Bus serial port 2 One port is provided for use with Air Data computer or Static Pressure Sensor interfaces This port is common with the Air Data RS 232 port described in Section 4 2 6 3 and can only function as a RS 232 interface or a RS 422 interface but not both Pin Assignment Signal Mnemonic Transmit A leg J2 27 ADC TXA Transmit B leg J2 44 ADC TXB Receive A leg J2 11 ADC RXA Receive B leg J2 10 ADC RXB 4 2 6 5 SCI Range RS 422 Digital Serial Bus serial port 1 Two ports are provided for use with the SCI range bus interfaces Port 1 is common with the ARINC 429 channel 1 port described in Section 4 2 5 and can only function as a RS 422 interface or ARINC 429 interface but not both Port 2 is common with the RS 232 port described in Section 4 2 6 4 and can only function as a RS 422 interface or an RS 232 interface but not both Pin Assignment Signal Mnemonic Receive A leg J2 36 429 422RX 1B Receive B leg J2 37 429 422RX 1A Receive A leg J2 10 232 422RX 2A Receive B leg J2 11 232 422RX 2B Note SCI Display Range RS 422 bus A and B legs are reversed from ARINC 429 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 169 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 2 7 Discrete Inputs Discrete signals are inte
207. N Note Not all of the following bits are necessarily used on a given aircraft but all will be processed The usage depends on the aircraft avionics For example Steep Approach is only supported in a limited number of installations however the bits for Steep Approach are always monitored 9 10 SDI 1 0 Left Display Range 0 1 Right Display Range 0 0 amp 1 1 No Range 11 14 Self Test command codes BIT 11 12 13 4 0 Test command 0 Short Level 1 Test command 0 Long Level 1 Test command 0 Level 2 Test command 0 Level 3 Test command 0 Level 4 Test command 0 Level 5 Test command 0 Level 6 Test command 1 Self Test Cancel command 0 0 1 1 Skip command or Ore 5 6 7 8 20 Weight Wheels Low Altitude momentary Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 289 Honeywell MK VI MK VIII EGPWS Installation Design Guide Timed Audio Inhibit momentary Reserved for EGPWS Test command Bit 24 9 12 224 Steep Approach activated alternate action 25 28 Terrain Display Range as specified in the table below BITS 25 to 28 Terrain Display Range 0 5 to 2000 NM format as follows DISPLAY RANGE BIT ASSIGNMENTS Bits 28 25 DEFINITION Bits 28 25 DEFINITION 2 6 2 49 Body Pitch Rate 326 Body Pitch Rate Source AHRS IOC LAB
208. NC 429 Low Speed Bus Basic 12 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B 2 40 Range Display Word 2 2 20 271 Discrete 5 320NM Basic N A 100 Auto Pop Up Category 7 Options Select Group 1 J1 32 GND DISC 12 au Display Select Discrete 1 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 Left Right shift keys on the display are not to be used when displaying terrain 2 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 210 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 12 Collins WXI 701 711 PPI without Auto Range Display Configuration Group 10 Display Type Collins WXI 701 711 PL o y Sweep Type Sene _ Peaks Mode Category 7 Options Select Group 1 5 3 7 Manual select
209. NC 429 Dual IOC buses Cat 9 ID 250 255 eene 96 S LIO ANSTFUCTIONS sce es COME cla a te 97 3 12 CATEGORY 10 ATTITUDE INPUT SELECT eene nnn ener nennen eren nennen enne 98 312 1 ROU ede emn ere th eed 98 3 12 2 Analog Pitch amp Roll Angle Synchro Cat 10 ID 0 2 4 98 3 12 3 Digital Pitch amp Roll Angle ARINC 429 High Speed Cat 10102586 99 3 12 4 Digital ARINC 429 Dual IOC buses Cat 10 ID 253 amp 59 99 I 99 3 1 HEADING INPUT UI EHE HU p ge ibis 100 3 13 T Magnetic Heading ee P eese rod eet gate Sau a Q EUR asa 100 3 13 2 Analog Heading Synchro Cat 11 ID 0 sse 100 3 13 3 Digital ARINC 429 AHRS Input Cat 11 ID 2 amp 3 101 3 13 4 Digital ARINC 429 Dual IOC buses Cat 11 ID 254 amp 255 nee 101 ILII ueni 101 3 14 CATEGORY 12 WINDSHEAR INPUT 5 0 102 Be LAT NO Windshear ui tiet em ete tiec ee ht ee e Sects as 102 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314
210. NITION BIT29 DEFINITION 0 O0 Failure Waming ____ ENS _ 0 1 __ Data NCD Right To Above 1 0 ___ Functional Test West BEN From Below BINARY CODED DECIMAL BCD DATA 0 O Plus North East Right To Above O 1 No Computed Data NCD 1 0 Functional Test Unless identified as using the Honeywell Discrete definition all data indicated as Discrete uses the following SSM definition Note that PWS uses a non standard SSM format as described in section 6 2 21 0 0 _ Normal Operation 0 1 NoComputed Data NCD 1 0 Functional Test_ Data identified as Honeywell Discrete uses the SSM definition below 0 0 _ Normal Operation 0 1 NoComputed DataNCD 1 0 Functional Test ISO 5 ALPHABET Some ARINC 429 labels transmit data using the ISO 5 alphabet as defined in the following table 2 2 000 991 009 211 190 NUL MCDU SELI MENU PROG SEL2 tpe rs sm L oe L 2 S 2 E Q gt AO un fo f s mr SEL RC E FPN 5816 SYN RAD NAV lt a FUEL NEXT PRED PAGE CLEAR LOGOFF SEL SERI F PLN 1 Jo fo 1 EVNT I Y SPARE SER l pe j a Zn gt Prop
211. P P TEST This assembly is illuminated with red background and activated during any Mode 1 Mode 2 or Terrain Awareness PullUp warning This assembly also includes a momentary switch that will activate EGPWS Self Test GLIDESLOPE alert Lamp Format 1 BELOW G S P CANCEL This assembly is illuminated with amber background and activated during any Mode 5 alert This assembly also includes a momentary switch that will de activate cancel EGPWS Mode 5 alerts during backcourse or low altitude approaches EGPWS caution Lamp Format 2 GPWS G S CANCEL This assembly is illuminated with amber background and activated during any EGPWS alert non Pullup This assembly also includes a momentary switch that will de activate cancel EGPWS Mode 5 alerts during backcourse or low altitude approaches Glideslope Canceled G S CANCLD optional but recommended This assembly is illuminated with white blue or amber background and activated after the flight crew has initiated the manual cancel of Mode 5 by pressing the BELOW G S P CANCEL light switch described above EGPWS Flap Override GPWS FLAP OVRD optional but recommended This guarded light switch assembly is illuminated with blue background and activated after the flight crew has initiated the manual selection of the GPWS Flap Override feature This assembly also includes a momentary switch that will activate GPWS Flap Override Note the light color may also be white background with black legend or b
212. PIN FUNCTION CONNECTION PIN TYPE DESIGNATION Polarity Configuration References REFERENCE Barometric Altitude 9 Input 28V_DISC_08 gt 17V Valid 6 6 22 Validity Discrete 28V lt 4 4V Invalid 42 7 Configuration Data Summary Data Derive Baro Altitude Rate Analog Baro Altitude Rate is derived using Uncorrected Barometric Altitude Although the ADC s provide Baro Rate the EGPWS does not have an analog connection available TABLE 5 3 2 13 AIR DATA INPUT SELECT 13 ed CONNECT TO ADC 1 Fault Designation AIR DATA BUS ed 2 Format ARINC 429 Low Speed Bus Tvpe Basic A J2 39 Data Reference Label Bits Range Signal Type Resolution Rate ms B 2328 Uncorrected Baro Alt 6 2 1 131 072 FT Basic 1 0 31 3 62 5 Outside Air Temp Outside Air Temp No Connection No temperature No temperature Computed Airspeed E Substitute Ground Speed for Airspeed airspeed is not available with this air data input Configuration Data Tye Summary Data Data Derive Baro Altitude Rate Digital Baro Altitude Rate is derived using Uncorrected Barometric Altitude Baro Rate is not available with this air data source Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 185 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 255 AIR DATA INPUT SELECT 255 CHANNEL CONNECT TO IOC 1 Fault Designation
213. PLAY BUS fault will be present only if both MG inputs have failed 3 The Honeywell EFIS SG amp MG provide Terrain display relay control 4 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 5 The display uses the following ARINC 429 labels from the EGPWS for annunciations The Terrain display will annunciate TERR in green or cyan depending on the program when the Terrain is selected and valid TERR in amber if Terrain is selected and any of the following conditions are TRUE e The EGPWS ARINC 429 output bus is missing or labels 050 and 051 are absent or unreadable for 2 seconds EGPWS ARINC label 051 bit 13 0 Terrain Display Valid bit FALSE EGPWS ARINC label 050 bit 17 1 Terrain Inhibit bit TRUE EGPWS ARINC labels are valid but the range in label 050 disagrees with the range via SCI bus label 80 label 050 bit 11 14 contain left display bus range and bits 15 18 are the right display bus range The display will be blanked when the amber TERR is present The display will Pop Up to Terrain mode as follows Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 227 Honeywell MK VI MK VIII EGPWS Installation Design Guide e the conditions indicated for the amber TERR above
214. PM Basic 16 0 31 3 62 5 Outside Air Temp Format DC Total Air Temperature 23 Input Type Basic Fault Designation STATIC AIR TEMPERATURE FAULT Probe element Excitation 5 V J1 25 2 J1 25 AA 5 V Ref Temp Input 1 63 4 42 probe element 44 63 3 Temp In 44 53 Chassis Gnd Ground GND J1 53 m oz yw tg lt ow Note Nominal 500 Temperature Probe only Resistance 0 C 5000 0 60 Connection example CIC Temperature Sensor P N 05257 2 wire Connect positive lead to both J1 25 and J1 63 Connect negative lead to both J1 44 and J1 53 Chassis Ground Other probes may have three contacts Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 183 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5 3 2 11 AIR DATA INPUT SELECT 11 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format DC with Validity Flag Uncorrected Barometric J1 62 6116 Input Basic Altitude gt 11 43 PE Fault Designation BAROMETRIC ALTITUDE FAULT Validity Barometric Alt Valid 28V Outside Air Temp Format DC Total Air Temperature Input Type Basic Fault Designation STATIC AIR TEMPERATURE FAULT Probe element Excitation 5 V 1 25 J1 25 AA 5 V Ref Temp Input J1 63 4 42 K Ohms probe element 1 44 63 Temp In 44 53 Chassis Gnd
215. Positronic Ind RD50F10JVLC 15 2 0 Configuration Module Honeywell 700 1710 020 This item may be available from Honeywell under Part No 440 1233 001 ITEM 2_ DESCRIPTION Connector P2 Positronic Ind PN RD50F10JVLC 15 is a packaged kit consisting of the following parts 1 1 Connector 50 socket D Sub Qty 1 1 2 Contacts size 20 crimp Qty 50 1 3 Backshell housing Qty 1 1 4 Backshell plate Qty 1 1 5 Screws Phillips CSK Qty 2 1 6 Spring Clip Qty 1 1 7 Slide Lock Qty 1 1 8 Screws Slotted Qty 2 1 9 Cable Clamp Qty 1 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 32 Honeywell MK VI MK VIII EGPWS Installation Design Guide INSTALLATION ASSEMBLY SEQUENCE STEP 1 Install all MK VI MK VIII system aircraft wiring to this connector using items 1 2 Crimp Contacts and item 1 1 Connector See figure 2 1 1 below I 2 C4 NU Or y 22 JA EN 5 C AN DG Od a 2 2 0 Ey 6 WwW n Ks N 2G 566 JV ON RON NV ane UE N es 9 EN 25 OW a ve 53 e 50 G N E La NO NO Q Ur 6 3 gt CM AT KON K 5 lt 3 6 6 Go x XG O 5
216. QNH Corrected Baro Alt relative to sea level RA Radio Altitude RAM Random Access Memory RDOP Radar Display Output Processing ROM Read Only Memory RTCA Requirements and Technical Concepts for Aviation RTS Ready to Transmit Signal RWY Runway S T Self Test S W Software SDI Source Destination Identifier SDRD Software Design Requirements Document SIG Significant SPC Stall Protection Computer SRD System Requirements Document SSM Sign Status Matrix ST Self Test SWC Stall Warning Computer TA amp D Terrain Awareness amp Display TACAN Tactical Air Navigation TAD Terrain Awareness Display TBD To Be Determined TCAS Traffic Collision Avoidance System TCF Terrain Clearance Floor TERPS United States Standards for Terminal Instrument Procedures TK Track TLB Translation Lookaside Buffer TSO Technical Standing Order TTL Tuned To Localizer UART Universal Asynchronous Receiver Transmitter USM Unsigned Magnitude UTC Universal Time Correlation UUT Unit Under Test VDC Volts DC VDOP Vertical Dilution of Precision VFOM Vertical Figure of Merit VHF Very High Frequency VLSI Very Large Scale Integrated Circuit VOR VHF Omni directional Range W S Windshear WC Warning Computer WGS 84 World Geodetic System 1984 ICAO Standard WX Weather Radar Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 326
217. RSPEED 19 WINDSHEAR WARNING THRESHOLD WINDSHEAR WARNING THRESHOLD COMPUTED BY EGPWS 9 COMPUTED CORRECTED LONGITUDINAL ACCELERATION RAW TOTAL SHEAR RAW TOTAL SHEAR COMPUTED BY _ P COMPUTED CORRECTED NORMAL ACCELERATION P gt COMPUTED CORRECTED FLIGHT PATH ANGLE 2 376 71215 SCALED TOTAL SHEAR SCALEDTOTALSHEARCOMPUTEDBYEGPWS P eiie i TERR AINDIPLAYOUTPUIS ___ S _ GE EMEND ee ee ee L _ ___ EQUoIMENTID 21 5 eee j FAUTSUMMARYWORDS S Lm 2 7 2 2 PEAKS ELEVATION BINARY pl ee 7 1 6 1 PEAKS UPPER ELEVATION UPPER ELEVATION VALUE AND COLOR 7 1 6 2 PEAKS LOWER ELEVATION LOWER ELEVATION VALUE AND COLOR NOTES 1 Update rate 100 ms 10 2 Update rate 200 ms 10 3 Update rate 500 ms 10 4 Transmitted only if Terrain Awareness function enabled 5 Update rate 1000 ms 10 6 NCD and Failure Warning Indications Provided 7 Transmitted only if Peaks enabled 8 Update rate 500 ms 10 for each SDI 9 Update rate 100 ms 20 Labels only used for testing Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 304 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 1 Discrete Output Words The discrete output words transmit the status of all MK VI and VIII EGPWC discrete
218. Radio Altitude Validity J1 29 Input 28V DISC 07 gt 17V Valid 6 6 1 Discrete 1 28V lt 4 4 Invalid 4 2 7 lt not gt Gnd Above DH 4 2 7 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 244 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 8 1 Radio Altitude Input Select Type 1 ALT 55 Format Alt 55 with Validity Flag Radio Altimeter 1 11 64 Input Type Basic J1 45 Fault Designation RADIO ALTIMETER FAULT Validity Radio Altitude Valid Discrete 1 28V REFERENCE Discrete 1 28V lt 4 4 Invalid 4 2 7 DH Discrete Gnd J1 33 Input GND_DISC_11 Gnd Below DH 6 6 14 lt not gt Gnd Above DH 4 2 7 Table 5 3 8 2 Radio Altitude Input Select Type 2 ARINC 429 CHANNEL CONNECT TO Left LRRA Fault Designation RADIO ALTIMETER BUS 429RX 5 Format ARINC 429 Low Speed Bus Basic B J2 4 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 REFERENCE DH Discrete Gnd J1 33 Input GND DISC 11 Gnd Below DH 6 6 14 not Gnd Above DH 4 2 7 Table 5 3 8 3 Radio Altitude Input Select Type 3 RT 200 300 Format DC with Validity Flag RT 200 300 Precision Output Radio Altimeter 1 11 64 Input Type Basic J1 45 Fault Designation RADIO ALTIMETER FAULT Validity Radio Altitude Valid Discrete 1 28V REFERENCE Radio Altitude Validity J1 29 Input 28V DISC 07 gt 17V Valid 6 6 1 Discrete 1
219. Resolution Rate ms J2 36 Range Mode Range Word 6 2 21 176 Discrete 5 640NM Basic N A 50 CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Mode Range Word 6 2 21 176 Discrete 5 640NM Basic N A 50 Output 429 Bus Group 1 Channel Pins Commens S 429TX 1 Low Speed Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x nl N 429TX_2 Low Speed A J2 26 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x B J2 9 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 The Terrain Display will Pop Up in response to EGP WS label 274 bit 28 left display and bit 29 right display 3 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGP WS Self Test 4 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 224 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3
220. S 4 A s R 17 Character Code Next Most of Set3of6_ 7 43 54 T 18 Character Code Next Most of Set 3of6 D 5 U 19 Character Code Next Most of Set3of6_ C 45 56 V 20 Character Code Next Most of Set 3of6 46 597 w 7 21 Character Code Next Most of Set3of6_ 7 72 6 SBE x 24 Character Code Next Most of Set 4of6 5 7 25 Character Code Next Most of Set 4of6 48 K s 26 Character Code Next Most of Set4of6 J L 5 7 27 Character Code Next Most of Set 4of6 402 5 O 28 Character Code Next Most of Set4of6 NOTE Text code for degree sign is non standard ASCII for 40pgx 7 1 3 6 Message Word 4 055 This label contains the last 2 characters to be displayed on the 6 character terrain display window Label Octal 055 Transmit Interval 200 msec 10 ______________ Cy BITNO DEFINITION dT BIT Coding J 910 8400 14 Lodo 414 12 15 14 13 Spre 2 2 1 1 Spare 14 5 Sere 4 1 16 Character Code Next Most of Set5of6 LSB 7bitHex 17 Character Code NextMostofSetSof6 18 Character Code Next Most of Set 5of6 19 _ Character Code Next Most of Set 5of6 20 Character Code Next Most of Set 5of6 21 Character Code Next Most of Set 5of6 P
221. SS CAUTION CAUTION TERRAIN PAUSE CAUTION TERRAIN 4 MODE 4 TOO LOW TERRAIN TOOLOWTERRAIN 1 TCF TOO LOW TERRAIN TOOLOWTERRAIN 1 Oo _____ pun MODE 6 ALTITUDE CALLOUTS SELECTED CALLOUTS MODE 4 TOO LOW GEAR TOO LOW FLAPS MODE 4 TOO LOW FLAPS TOO LOW FLAPS MODE 1 SINKRATE SINKRATE 5 Note The basic warning is SINKRATE PAUSE SINKRATE However if the Mode 1 Pullup curve is violated only a single Sinkrate may occur prior to the pull up voice MODE 3 DON T SINK DON T SINK PAUSE DON T SINK MODE 5 GLIDESLOPE GLIDESLOPE MODE 6 BANK ANGLE BANK ANGLE PAUSE BANK ANGLE 5 BANK ANGLE BANK ANGLE Honeywell Algorithm low altitudes MODE 7 WINDSHEAR CAUTION QUIET or CAUTION WINDSHEAR if Caution voice Enabled Note 1 These the only voices that can interrupt Note 2 The preface voices will always be given prior to the warning voice Note 3 Voice message is continuous Note 4 Voice message will repeat every 10 seconds Note 5 Long Self Test will only issue a single Sinkrate Note 6 The Windshear Alerts will only be given on a MK VIII EGPWS with Windshear enabled per Category 12 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 196 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 5 3 Audio Menu Type 3 Alternate for Fixed Gear Aircraft 7 WINDSHEAR WARNING _ SIREN WINDSHEAR W
222. Signal Type Resolution Rate ms CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Tvpe Basic J2 40 Range Mode Range Word 6 2 21 176 Discrete 5 640NM Basic N A 50 Output 429 Bus Group 1 Chanel Comments 429TX_1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x and 7 1 6 B J2 42 429 2 Low Speed A J2 26 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x and 7 1 6 B J2 9 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 The Terrain Display will Pop Up in response to EGP WS label 274 bit 28 left display and bit 29 right display 3 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGP WS Self Test 4 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 223 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 241 Collins Pro Line 21 Integrated with binary Peaks Elevations MK VIII Only and Full Compass Raster Patch Display Configuration Group 247 Function Reference sec
223. Spec 14 is in process 6 20 x 3 04 x 10 30 3 9 pounds maximum Standard 3 inch King Radio rack 55 C to 70 C F2 55 000 feet F2 No cooling necessary No shock mounting required 2 5 Amps max 9 watts no warning 7 watts with warning over 8 ohm speaker 3 watts with GPS card 49 watts with heater blanket on Configuration Module TSO Compliance Physical size Weight Mounting Temperature operational Altitude range Cooling Shock Power Consumption 5 VDC TSO C151b 2 68 x 1 51 x 0 32 fits Positronic connector backshell 1 pound with connector and backshell Mounts to Positronic connector backshell same as MK VI MK VIII EGPWS same as MK VI MK VIII EGPWS No cooling necessary No shock mounting required from MK VI MK VIII EGPWS GPS Antenna Sensor See Section 1 5 4 ARINC 743A TSO C129A and Manufacturer s specifications OAT Sensor Nominal 500 ohm Temperature probe resistance at 0 C 500 ohm 0 6 ohm Range 70 C to 60 C reference ARINC 575 Section 3 8 or ARINC 706 Section 4 8 See Manufacturer s specifications 1 7 Units Supplied 1 7 1 MK VI EGPWS The MK VI EGPWS is available in two versions with internal GPS card or without The part number for the units is as follows 965 1180 XXX without internal GPS card 965 1190 XXX with Internal GPS card Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG
224. Speed Bus Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 41 Radio Altitude 6 2 29 164 16 8192 FT Basic 0 125 25 50 B J2 40 REFERENCE DH Discrete Gnd J1 33 Input GND DISC 11 Gnd Below DH 6 6 14 not Gnd Above DH 4 2 7 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 246 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 8 254 Radio Altitude Input Select Type 254 ARINC 429 via dual IOC buses CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 1 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Radio Altitude 6 2 29 16 8192 FT Basic 0 125 25 50 Decision Height format 3 6 2 41 16 8192 FT Basic 0 125 100 200 MDA format 3 6 2 51 16 565536 1 0 200 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Radio Altitude 6 2 29 16 8192 FT Basic 0 125 25 50 Decision Height format 3 6 2 41 16 8192 FT Basic 0 125 100 200 MDA format 3 6 2 51 16 65536 Basic 1 0 200 Table 5 3 8 255 Radio Altitude Input Select Type 255 ARINC 429 via dual IOC buses CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 1 Format ARINC 429 High Speed Bus Type
225. T 22 __ Character Code Next Most of Set 5of6 MSB 7bitHex 23 Character Code Right Most of Set6of6 LSB 7bitHex J 24 Character Code Right Mostof Set6of6 T O 25 Character Code Right Most of Set6of6 7 26 _ Character Code Right Most of Set6of6 27 Character Code Right Most of Set6of6 28 Character Code Right Most of Set6of6 29 Character Code Right Most of Set 6 of6 MSB 7bitHex Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 312 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 4 Equipment Identification Provides equipment identification for maintenance reporting 7 1 4 1 Equipment Identification Word 377 E o aa e SS c BIT DEFINITION 11 22 ID Code Equipment ID code 023 Hex for EGPWC 7 1 5 Fault Summary Words for Proline 4 21 Provides fault diagnosis information 7 1 5 1 Fault Diagnostic Word 1 350 Label Octal 350 Transmit Interval 1000 msec 10 Data Discrete BIT 11 12 13 14 15 16 17 18 t2 ro gt 5 DEFINITION 1 ARINC 429 INPU ARINC 429 INPU ARINC 429 INPU ARINC 429 INPU ARINC 429 INPU ARINC 429 INPU ARINC 429 INPU ARINC 429 INPU Failed T 1 FAILED T 2 FAILED T 3 FAILED T 4 FAILED T 5 FAILED T 6 FAILED T 7 FAILED T 8 FAILED NALOG DC INPUT 1 FAILED
226. TE APPROVED SHEET NUMBER Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 3 Honeywell MK VI MK VIII EGPWS Installation Design Guide THIS PAGE INTENTIONALLY LEFT BLANK Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 4 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE OF CONTENTS SECTION I GENERAL INFORMATION 13 TEINTRODUCTIONS irat ee deep Qai iet dod te e e ater ur t p 13 APPEICABIDLITY ree ERE en ma keq 13 TOUSE THIS c eee n pere eerte eroe rapax ee L 13 IA REFERENCE DOCUMENTS its irte irt ite ire a ue erano nei m att n Oe PH 14 1S DESCRIPTION OF EQUIPMENT te teet ete e ier e alt 15 15 1 MK VI EGPWS Computer deer recede ng a EEE 15 1 5 2 MK VIII EGPWS Computer eene eene nter eren rre eere 15 1 5 3 MK VI MK VIII EGPWS Configuration Module seen 15 I 3 4GPS Antenna Gnd Gadling et vives m tdt deed ete edet ated nu 16 OATH SCUSOP DT 17 1
227. TEGORY 13 INPUT OUTPUT DISCRETE TYPESELECT usan sauna eene nennen 103 3 13 1 eite d et 103 3 15 1 1 Glideslope Inhibit Discrete a ua Qatun Quq quas 103 3 15 12 Landing Discrete potete be ette au u e S Re aa Gas 103 3 15 1 3 Audio Inhibit Discrete EP REI Landing Gear Discrete Em 104 3 15 1 5 Glideslope Cancel Discrete 106 3 15 1 6 Momentary Flap Override Discrete eee eee esee eee E 106 3 15 1 7 Mode 6 Low Volume Discrete ee d e m a Rar E eg 106 3 15 1 8 Autopilot Engaged Discrete nn ener enne tnst enne entrent enne nnne 107 3 15 1 9 Terrain Awareness and TCF Inhibit Discrete eren eene rennen trennen ener teen 107 3 15 T 10 Self Test Discrete cus aee Dh epe oen ede te de e el 107 3 15 1 Steep Approach Discrete 9 2 u ids E dS eka edet A Ou S baa eA Wa aie ORE ERSTE 108 3 15 1 12 GPWS INHIBIT Discrete alternate action cccecccssessseeecesecsseeseesecaecseeeseeseeseceaecaeeeseeseceaecaeeeseeseceaecaeeeseeeeeaecneeeeees 108 3 15 2 Ouiput Discretes o IR toti alli a Sides e ps W ue ee li in 108 3 152 1 La
228. TY FAULT gt 0 145V Valid typical active range is 0 16V to 0 84V lt 0 145V Invalid PIN FUNCTION CONNECTION PIN TYPE CHANNEL DESIGNATION Polarity Configuration Reference REFERENCE 28V ILS Tuned J1 39 Input 28V_DISC_01 gt 17V ILS Tuned 6 6 9 Discrete 1 lt 4 4V ILS Not Tuned 4 2 7 GND ILS Tuned J1 20 Input GND DISC 01 Gnd ILS Tuned 6 6 8 Discrete 1 lt not gt Gnd ILS Not Tuned 4 2 7 Table 5 3 9 2 Navigation Inputs Select 2 CHANNEL CONNECT TO ILS 1 Fault Designation ILS BUS 429RX 6 Format ARINC 429 Low Speed Bus Basic A 12 22 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 5 Glideslope 6 2 30 174 12 0 8 DDM Basic 0 0001953125 33 3 66 6 Table 5 3 9 3 Navigation Inputs Select 3 CHANNEL CONNECT TO ILS 1 Fault Designation ILS BUS 429RX 6 Format ARINC 429 Low Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms J2 22 Glideslope 6 2 30 174 12 0 8 DDM Basic 0 0001953125 33 3 66 6 J2 5 Localizer 6 2 33 173 12 50 4 DDM Basic 0 00009765625 33 3 66 6 Glideslope Deviation Low Level Glideslope 11 30 Deviation Validity 1 10 Table 5 3 9 4 Navigation Inputs Select 4 CHANNEL CONNECT TO ILS 1 Fault Designation ILS BUS 429 6 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Signal Type Resolution Rate ms Glideslope 6 2 30 Basic 0 0001953125 33 3
229. The Bank Angle feature provides protection for over banking during maneuvering on approach or climb out and while at altitude In addition it protects against wing or engine strikes close to the runway For airplanes fitted with an autopilot additional protection is provided if the autopilot is engaged by advancing the roll angle limit to 33 degrees The additional autopilot engaged protection applies to all software versions for GA FAST and GA SLOW aircraft types whereas it is available in software version 008 or later for Bizjet aircraft types The Bank Angle callout can be enabled or disabled as appropriate for this installation 3 9 6 Flap Revers al The Landing Flap discrete input is defined in Category 13 The Category 7 control is used to reverse the defined logic to match aircraft wiring if necessary 28 VDC Landing Flap discrete J1 37 active position Flap Reversal Flap Discrete Category 13 False True Landing Flap discrete 28V Flaps Up Flaps Down Landing Flap Discrete Open or GND Flaps Down Flaps Up Ground seeking Landing Flap discrete J1 18 active position Flap Reversal Flap Discrete Category 13 False True Landing Flap discrete GND Flaps Up Flaps Down Landing Flap Discrete Open or 28V Flaps Down Flaps Up 3 9 7 GPS Altitude Reference The GPS Altitude ARINC 429 label 076 Category 3 may be referenced to mean sea level MSL or WGS 84 Determine which ref
230. This discrete is typically connected to an alternate action switch in the cockpit The recommended label for this switch is Terrain Override although labeling for this switch should be consistent with existing cockpit nomenclature Terrain Inhibited will be annunciated during cockpit Self Test if these functions are inhibited Discrete Position Status Connector Pin TA amp TCF Inhibit Inhibit Gnd Not Inhibit Open J1 12 3 15 1 10 Self Test Discrete The cockpit Self Test discrete is provided to manually initiate test of the EGPWC EGPWS aircraft interface and to enunciate system configuration and status information This discrete is typically supplied by a momentary action cockpit push to test switch typically part of the GPWS WARN Lamp assembly This discrete must be momentarily connected to ground to activate the Self Test Activation of this discrete continuously for more than 60 seconds will result in the Self Test Invalid fault which will cause a GPWS INOP indication Discrete Position Status Connector Pin Self Test Self Test Gnd Normal Open J1 34 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 107 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 15 1 11 Steep Approach Discrete 2 For some installations a Steep Approach bias can be optionally appl
231. VI MK VIII EGPWS CONFIGURATION MODULE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 38 Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 7 Secure Configuration Module to connector assembly using item 1 5 Screws as shown in figure 2 1 7 below Tighten Cable Clamp screws as required ITEM 1 5 Screw 2 Places 2000000 9 9 9 A CONFIGURATION MODULE 9 f NU e FRONT VIEW FIGURE 2 1 7 MK VI MK VIII EGPWS CONFIGURATION MODULE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 39 Honeywell MK VI MK VIII EGPWS Installation Design Guide 2 3 6 GPS Antenna location The GPS antenna should be mounted on top of the fuselage in the centerline of the aircraft Avoid mounting the antenna near any projections the propeller and the T tail of the aircraft where shadows could occur It is recommended that there be a separation of at least 3 feet between the GPS antenna and any VHF Comm antenna on the aircraft The GPS antenna baseplate must be level within 5 in both axis when the aircraft is level level is defined as the aircraft attitude requi
232. Y 70 ia oz ly Ul 549 627 ni 225 dd Sdo 9 ul L 62 SNO ely STX SN9 sMdos3 cr Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 72 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide 098 099 0FS GINM PSA L 0vSQIADI uoneuluu 8 Ul 88457 y g V 098 099 0 9 INO 1000 80901 900 N d lenuew uoneljejsu 295 0S9 0SS 0rS QNM eui jo pue 103 JON uonov leus lv sng due 1591 duie1 uonoeuuoo ON J8je JO 020 0 21 996 IIIA MIN J8je JO 020 0X 11 496 IA 1n0 uqiuu uresa L g V g V INO Z O9PIA 8dOM INO L O9PIA 8dOM ul zit ONIHV ul ONIHV SMd93 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 73 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide VSt VH L PSNGEVH L cX SvIS 08 uoneuiuuo 0 8 ul V 8 V jno eBues 97 19 08 uoneuruuo 0 8 ul V 8 V jno eBues LO Ob ve
233. ZE A DWG 060 4314 150 REV 1 1 1 1 1 SHEET 319 Honeywell MK VI MK VIII EGPWS Installation Design Guide Connector Channel Pin Designation Signal Usage Summary Reference J1 49 DISC_OUT_9 Terrain Select Relay Output 2 J1 50 MON OUT 3 Windshear INOP Lamp Output monitor J1 51 DISC OUT 8 Spare Lamp Output J1 52 Steep Approach momentary Lamp Output or 782 Windshear Caution Lamp Output J1 65 GSDEV_H Glideslope Deviation Low Level up J1 66 J1 63 OAT_H Air Temperature i J1 64 RALT_H Radio Altitude ARINC 552 or ALT 55 3 J1 68 28V DISC 12 Attitude Validity Discrete 28VDC J1 70 AUD HL H High Level Audio Output 80 J1 72 MON 1 GPWS INOP Output monitor J1 73 Flap Override Output Gnd or MIGNE DISCUS Windshear Warning Output 1 71 AUD HL L High Level Audio Output 80 J1 74 AUD LL L Low Level Audio Output 6000 dL 1 69 DISC_OUT_5 Audio On GND Output J1 75 AUD_LL_H Low Level Audio Output 600Q J1 76 DISC_OUT 3 Glideslope Cancel Output J1 77 DISC_OUT 2 Glideslope Alert Output J1 78 DISC_OUT_1 GPWS Warning Output a 0 ________ 42 01 SYN 4X Configurable Synchro 1 X leg J2 02 SYN 4Y Configurable Synchro 1 Y leg J2 03 SYN 5Z Configurable Synchro 2 Z leg J2 04 429RX_5B Radio Altitude ARINC 429 Input B leg 2 06 429RX 7B AHRS ARINC 429 Input B leg GPS 2 ARINC 429 Input B leg
234. ____ MODE 6 ALTITUDE CALLOUTS SELECTED CALLOUTS MODE 4 TOO LOW GEAR TOO LOW GEAR MODE 4 TOO LOW FLAPS TOO LOW FLAPS MODE 1 SINKRATE SINKRATE 5 Note The basic warning is SINKRATE PAUSE SINKRATE However if the Mode 1 Pullup curve is violated only a single Sinkrate may occur prior to the pull up voice MODE 3 DON T SINK DON T SINK PAUSE DON T SINK MODE 5 GLIDESLOPE GLIDESLOPE YV UP MODE 6 BANK ANGLE BANK ANGLE PAUSE BANK ANGLE BANK ANGLE BANK ANGLE MODE 7 WINDSHEAR CAUTION QUIET or CAUTION WINDSHEAR if Caution voice Enabled Note 1 These are the only voices that can interrupt Note 2 The preface voices will always be given prior to the warning voice Note 3 Voice message is continuous Note 4 Voice message will repeat every 10 seconds Note 5 Long Self Test will only issue a single Sinkrate Note 6 Windshear Alerts will only be given on a MK EGPWS with Windshear enabled per Category 12 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 194 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 5 1 Audio Menu 1 Alternate MODE 7 WINDSHEAR WARNING 6 WINDSHEAR WINDSHEAR WINDSHEAR 6 X i MODE 4 TOO LOW TERRAIN TOOLOWTERRAIN 1 TOO LOW TERRAIN TOOLOWTERRAIN 1 MODE 6 ALTITUDE CALLOUTS SELECTEDCALLOUTS ___
235. a loCation E cine 40 2 3 7 GPS Antenna Installations u S Ss ales page Su BEES RR m ee sie Wu 40 OQ AT SCHSOPEOCQHOM MIA h 40 2 3 0 OAT Sensor Installations RENE ER 40 DEB I0 Cockpit Lights rte e estt ie e ee reete oe 40 2 3 T0 lE DOseriptrionm ott pe ater E Ee bids UE EH E 41 2 3102 Location M 42 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 28 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION Il INSTALLATION 2 1 Introduction This section contains suggestions and factors to consider before installing the Enhanced Ground Proximity Warning System Close adherence to these suggestions will assure satisfactory performance from the equipment NOTE The conditions and tests performed on this article are minimum performance standards It is the responsibility of those desiring to install this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within these performance standards The article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the airworthiness authority 2 2 Unpacki
236. aaah leg ee Prae ates 89 3 9 6 Flap REVErS Al vs zh t tiae ae edad tei eee 8 amp 9 3 9 2 Refevengeau aaa d rete 89 ILIS INSU ONS a ma a aa ere gre e 90 3 10 CATEGORY 8 RADIO ALTITUDE INPUT SELECT sseseesseeeee eee n nennen nennen nn nnne trennen 91 3410 1 Radio Altitude Input 5 aee de e eee ett t d hte eno 91 3 10 2 Decision Height Discrete Input eee eene entrent ener erre 91 3 10 3 Digital Radio Altitude Interface Cat 8 ID 2 sees 91 3 10 4 Analog Radio Altitude Interface Cat 8 ID 0 1 3 4 sess 92 3 10 5 Digital ARINC 429 Dual IOC Buses Cat 8 ID 251 255 92 3 40 C IRSIFAGHORS is stitit acce n eet c d ee n ee eec t e eee re Edere 93 3 11 CATEGORY 9 NAVIGATION INPUTS 94 3 11 1 Navigation Inputs Select Glideslope amp Localizer Inputs esee 94 34 L2 Glideslope Validity us saa m a S o ete unanqa ut 94 24 23 Eocalizer Validity x e orn be RS OU ARR De ete u ua 94 3 11 4 ILS Tuned Discrete Input 1 280 and 2 2 22222 20 00000000000000 00000 eene 94 3 11 5 Analog Glideslope Interface Cat 9 ID 0 1 5 sse eene 95 3 11 6 Digital Glideslope Localizer ILS Select Interface Cat 91023 96 3 11 7 Digital ARI
237. aircraft systems Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 316 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 4 11 Windshear Caution The MK VIII EGPWC Windshear Cautions can be configured to activate any of the discrete outputs Depending on configuration the Caution discrete will typically drive its own output lamp or provide a discrete output to other aircraft systems 7 4 12 Steep Approach Discrete The Steep Approach discrete is active whenever Steep Approach has been selected via the pilot or an Envelope Modulation steep approach case is active and is typically used to drive a lamp in the Steep Approach switch For standard steep approach selection method alternate action switch this discrete is not provided as the switch must be self lighting For Discrete I O category IDs that supply a momentary Steep Approach Switch this lamp driver output is provided to light the switch 7 5 System Configuration Status The EGPWC indicates the current hardware software databases Category states and input discretes detected by the system Each configuration item has an associated configuration message This is the message that will be read out during Present Status on the 5 232 interface or voice output during Self Test Level 3 to inform the user of the current configuration TABLE 7 5 1 CONFIGURATION OPTIONS AND MESSAGES TERRAIN CLEARANCE FLOOR DISABLED
238. al ARINC 429 Dual Buses Cat 8 ID 251 255 Radio Altitude Type 251 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 164 and 170 Radio Altitude Type 252 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 164 and 370 Radio Altitude Type 253 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having label 164 and a analog discrete DH input Radio Altitude Type 254 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 164 170 and 370 Radio Altitude Type 255 IOC bus or equivalent is a dual high speed digital ARINC 429 signal having labels 164 and 370 For interface description see paragraph 3 4 5 Air Data Type 255 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 92 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 10 6 Instructions Using Appendix E Tables 5 2 5 3 8 and 5 3 8 x as described above select the Radio Altitude Input Type that matches the aircraft configuration features preferences and version part number being installed Record the ID number for the Radio Altitude Type from Appendix E Table 5 3 8 under the Ident No heading for Step Category 8 in Appendix E Table 5 2 Using the Radio Altitude Type number from Appendix E Table 5 3 8 as x go to Appendix E Table 5 3 8 The electrical interfaces pin outs for Radio Altitud
239. alid gt Attitude Valid Invalid gt Attitude Invalid Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 301 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 6 25 Steep Approach Discrete 2 Activates steep approach biasing if Steep Approach Enabled is true see Category 7 Section 5 3 7 Alt Action Type Supplied by an alternate action latching and self indicating cockpit switch Momentary Type Supplied by a momentary non latching switch with switch lamp driven by EGPWS Steep Approach Discrete output Signal Status Steep Approach Selected or not Selected Fault monitoring None if Steep Approach Enabled is false EGPWS Self Test is inhibited if Steep Approach Enabled is true and Steep Approach Discrete 2 is Selected on the ground For momentary switch inputs activation of this switch input for more than 15 seconds will result in the Steep Approach Invalid fault which will cause a GPWS INOP indication Level 6 Audio readout Steep Approach Discrete 2 Selected gt Steep Approach Selected Not Selected gt Steep Approach Not Selected 6 6 26 Timed Audio Inhibit Discrete Type Supplied by a momentary action internally latching and indicating cockpit switch for inhibit of audio functions Signal Status Audio Inhibit or not Inhibit Fault monitoring The Audio Inhibit function does not inhibit Self Test ther
240. allation Design Guide External Validity Flag Connection AIC LSB 0 03125 C AIC Status Mask 00000000 External Validity Type 6 1 6 ARINC 547 578 4 Low Level Glideslope Deviation with Discrete Valid Signal Name Low Level Glideslope Deviation DC Signal DC Absolute 16 Dots 12 Dots 15 Dots None None Scale GS Deviation Dots 13 333333 Dots VDC Volts Positive Fly Down 75 mV per DOT 0 Volts 0 DOT NOTE To be consistent with the ARINC 429 definition G S scaling inverts sign of input signal such that positive numbers are fly down Input Signal Connection J1 65 above beam J1 46 below beam Input Reference Connection None AIC Name D3 DC3 J1 11 28 VDC discrete 0 00048828 Dots 0000200C Discrete Validity 6 1 7 ARINC 547 578 4 Low Level Glideslope Deviation with Low Level Valid Signal Name Low Level Glideslope Deviation DC Signal AIC Algorithm DC Absolute Scale GS Deviation Dots 13 333333 Dots VDC Volts Positive Fly Down 75 mV per DOT 0 Volts 0 DOT NOTE To be consistent with the ARINC 429 definition G S scaling ERN inverts sign of input signal such that positive numbers are fly down Input Signal Connection J1 65 above beam J1 46 below beam None 1 30 gt J1 10 GS low level validity see 6 1 21 6 1 8 Roll Attitude 3 Wire Synchro 11 8 VAC Signal Name Roll Attitude 3 Wire Synchro AIC Algorithm 3 Wire Syn
241. an be rewritten using the CUW command as before or individual categories can be changed as follows 4 Atthe CFG prompt use the CAT command with the following structure CAT lt space gt lt category gt lt space gt lt ID gt lt space gt lt T or F gt lt Enter gt category gt is the Appendix E Category to change example 7 lt ID gt is the new ID to change to example 92 lt T or F gt is True or False for rebooting the EGPWC Use if only one category is to be changed and the EGPWC will reboot following Enter Use F if another individual ID is to be changed by another CAT operation Example gt CAT 7 92 T lt Enter gt 5 After inputting the desired change information pressing Enter will transmit the data to the EGPWC to write to the Configuration Module If a reboot is commanded T then the EGPWC will reboot at the completion of the write process If a reboot is not commanded F then a message Writing to configuration module Category 7 ID updated successfully is given and the CFG prompt is again displayed At this point the Configuration Module has been changed but the change will not be effective until the EGPWZC is rebooted Additional changes can be made with the final change set to command the EGPWC to reboot or cycle EGPWC power to reboot 6 Verification of the changes made is the same as before As above type CFG to restart the Configuration sub mode At C
242. ance Z leg Maximum Reverse Fault Current Input Voltage Range Accuracy 4 2 4 1 Synchro Roll Attitude Quantity Synchro Angle Range Reference Voltages Pin Assignment Signal Mnemonic X leg Y leg Z leg Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A 2 gt 83 lt 200 uA 5 VDC 0 1 Second Low Pass 10 Differential Input will be biased less than 6 VDC 71 26 J1 27 J1 66 J1 47 gt 140 gt 140 gt 140 lt 200 HA 11 8 VACgys 20 leg to leg 2 5 linearity 0 1 full scale offset 1 80 deg Not Required 11 1 5 1 11 21 SYN 1Y 11 2 SYN 17 DWG 060 4314 150 REV SHEET 166 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 2 4 2 Synchro Magnetic Heading Quantity Synchro Angle Range Reference Voltages Pin Assignment Signal Mnemonic X leg Y leg Z leg 4 2 4 3 Synchro Pitch Attitude Quantity Synchro Angle Range Reference Voltages Pin Assignment Signal Mnemonic X leg Y leg Z leg 4 2 4 4 Configuration Defined Synchro Inputs Quantity Reference Voltages Pin Assignment Signal Mnemonic 2 X leg 2 Y leg 2 Z leg 3 X leg 3 Y leg 3 Z leg 4 2 4 5 Signal Timing Reference Inputs 1 180 deg 26 VACpms 20 see 4 2 4 4 J1 22 J1 23 J1 3 1 80 deg Not Required J1 5 2 26 VACpms 20 1 2 J2 18 J2 19 J2 20 J2 3 SYN_2X SYN_2Y
243. and audio outputs Label 274 is typically used to drive EFIS and or EICAS displays The other discrete labels are typically only used for flight recording and test purposes 7 1 1 1 EGPWS Alert Discrete 1 270 Data ignificant Bits ign Bit 20 22 26 a b EE 5 Lm 5 2 100 msec 10 MINIMUMS MINIMUMS TERRAIN PULLUP CAUTION TERRAIN TERRAIN AHEAD PULL UP or OBSTACLE AHEAD PULL UP SIREN WINDSHEAR WINDSHEAR WINDSHEAR CAUTION WINDSHEAR ENGINE FAIL VEE CAUTION TERRAIN or TERRAIN AHEAD CAUTION OBSTACLE or OBSTACLE AHEAD OBSTACLE OBSTACLE 2 am NOTE Bits 23 through 26 will be set to zero when unsupported Bit 22 This bit is used for the alternate terrain and obstacle warning voice message The basic terrai n warning message is mapped to bits 13 and 12 and obstacle warning voice mapped to bits 29 and 12 Bits 23 amp 24 are supported by MKVIII EGPWS only provided that WS is included in configuration Bits 20 25 amp 26 are Not supported Bit 27 is the alternate Terrain Caution voice 7 1 1 2 EGPWC Logic Discretes 271 Data Label Significant Bits Sign Bit Transmit Interval BIT No 11 12 13 14 15 16 18 19 21 NOTE Bits 11 12 1 configuration Proprietary notic CAGE CODE 97896 100 msec 10 IDEFINITION 6 17 26 and 29 will be set to zero when Not Supported Supporte
244. ange MK VIII Only Display Configuration Group 239 Display Type 7 Honeywell Non Integrated EDZ806 __ f Auto Pop Up Peaks Mode Elevations via overlay Honeywell 4 2 2 31 Category 7 Options Select Group 1 5 3 7 No Yes a magenta underline will be alternately placed and removed under the Peaks Elevations Yes for Peaks Elevations located near the vertical center on the right edge of the Terrain image Honeywell picture bus CONNECT TO 453 1 58 Terrain Display data to switching relay Symbol Generator 1 J1 59 DISPLAY BUS 2 CONNECT TO 453 2 A J1 56 Terrain Display data to switching relay Symbol Generator 2 4 2 13 2 1 57 7 2 Display Input Control Group 249 CHANNEL CONNECT TO SCI Bus 1 Fault Designation DISPLAY BUS 1 429 422RX 1 Format RS 422 12 0 baud Bus Type Basic J2 36 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms 2 37 Range Mode Range word 6 5 1 1 80 4 discrete 2000NM Basic N A 100 Status 6 5 1 2 FF Discrete N A Basic N A 100 CHANNEL CONNECT TO SCI Bus 2 Fault Designation DISPLAY BUS 2 429RX 3 Format RS 422 12 0K baud Bus Type Basic 2 10 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 11 Range Mode Range word 6 5 1 1 80 4 discrete 2000NM Basic N A 100 Status 6 5 1 2 FF Discrete N A Basic N A 100 Polarity Configuration Type 1 Momentary CONN
245. ans to press and hold the ST button for more than 0 5 seconds but less than 2 seconds The procedure guides the operator directly to ST Level 3 System Configuration skipping most of ST Level 1 and Level 2 To verify the Regional Terrain Database that was just loaded into the EGPWC perform these steps NOTE On the Bench this test requires an audio speaker and a self test button These may not be available On the Bench unless when using a Break Out Box 1 Ensure the EGPWC power is ON 2 Press ST button to initiate ST Level 1 3 After ST Level 1 message starts Press ST button to cancel Level 1 and start Level 2 4 After ST Level 2 message Current Faults is heard Press ST button to cancel Level 2 5 When the message Press to Continue is heard Press ST button to start ST Level 3 6 Verify the Terrain Database version annunciated in the following sequence Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 125 Honeywell MK VI MK VIII EGPWS Installation Design Guide SYSTEM CONFIGURATION PART NUMBER 965 11 0 c MOD STATUS xx SERIAL NUMBER APPLICATION SOFTWARE VERSION f TERRAIN DATABASE VERSION The following example of Terrain Database Version annunciation 419A for ATLANTIC 419P for PACIFIC or 419N for AMERICAS Other versions
246. are being pressed will be represented as logic 1 in the appropriate bit while non pressed keys will be registered as logic 0 For a detailed description of the Key Press Display Mode Label 012 definition see the EGPWS Interface Methodology 060 4303 000 Approx LSB N A Sign Bit N A Key press Display Mode data will be transmitted using Label 012 This is an optional label for KCPB displays The state of the front panel keys will be transmitted nominally every 200 ms Keys which are being pressed will be represented as logic 1 in the appropriate bit while non pressed keys will be registered as logic 0 For a detailed description of the Key Press Display Mode Label 012 definition see the EGPWS Interface Methodology 060 4303 000 6 2 26 Control Word 1 270 WXR Control Panel Approx LSB N A Sign Bit N A 19 21 Tilt 4 0 degrees 0 0 0 0 0 y 1 12 13 14 1 1 1 1 5 6 7 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 284 Honeywell MK VI MK VIII EGPWS Installation Design Guide Bits 14 to 16 Mode format as follows __ _ 0 0 J Stndy 92292024 c O 1 PL 0 L0 1 WindshearHazardFactor _ gt 05 3 E 1 0 1 Windshearand Turbulence L1 Weather and Turbulence 6 2 27 Discrete Word 273 Bendix Weather Radar
247. asic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CONNPINZ REFERENCE NAME PIN FUNCTION Polarity Configuration J1 32 GND DISC 12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 Peaks Elevations are transmitted digitally to the display via Label 025 on the ARINC 453 bus They are then displayed as stroked characters on the bottom left or right of the display depending on EFIS strapping 2 Pop Up the Terrain display for a Terrain Caution or Warning it is necessary for the EFIS to receive two discrete signals from the EGPWS one to indicate that the Terrain display is selected and one to indicate that selection was due to an alert The EFIS needs to distinguish between manual selection and alert conditions so it will know when it should autorange Both EFIS and EGPWS start to autorange on a Caution or Warning to minimize any latency problem displaying status during an alert 3 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels T
248. at ARINC 429 Low Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Display Word 2 2 20 271 Discrete 5 320NM Basic N A 100 CONN PIN REFERENCE NAME PN FUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 205 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 7 Honeywell Bendix IN182A IN812A RDR 2000 RDS 81 82 Display Configuration Group 4 usss RDR 2000 and RDS 81 82 radar systems kr t Auto Pop Up 53 7 proper mode Peaks Mode Category 7 Options Select Group 1 5 3 7 Peaks Enabled False Peaks Enabled True Manual select
249. ate Pop Up False TA amp D Alternate Pop Up True Category 7 does not affect pop up logic The display controls pop up therefore enable disable of pop up is done via the display Peaks Mode Category 7 Options Select Group 71 5 3 7 C Manual select Selection is controlled by display __ Manual deselect Deselection is controlled by display 2222 Auto Range YeslONM 12 MovingMarker Yes for Peaks Elevations only located on lower right side of display p Display Priority Standard Honeywell picture bus DISPLAY BUS 1 amp 2 CONNECT TO 453TX 1 Honeywell left right interleaved picture bus to MFD and PFD 4 2 13 2 7 2 JI 58 71 59 7 CONNECT TO ur Not supported for this display type Display Input Control Group 250 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Sig Bits Signal Type Resolution Rate ms FWC amp GP discrete word 6 2 48 Format 1 Typel Basic N A 100 Bits 15 18 2000NM Bits 25 28 Discrete CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms FWC amp GP discrete word 6 2 48 Format 1 Typel Basic N A 100 Bits 15 18 2000NM Bits 25 28 Discrete Output 429 Bus Group 0 Channel Pins Comments 429TX 1 L
250. ated MK VIII Only Function Reference section Display Type Collins ProLine 21 Integrated with binary peaks elevation with partial compass raster patch Sweep Type Fan Mode with 90 degree limit Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Category 7 does not affect pop up logic The display controls pop up therefore enable disable of pop up is done via the display Display Configuration Group 254 Peaks Mode 5 3 Peaks Enable True Peaks On Manual deselect Deselection is controlled by display Yes 10NM Controlled by ProLine 21 system Moving Marker N 257 G Overlay Page FIND eee _ Display bus type ARINC compatible format Collins ProLine 21 label 077 YV yc Terrain Mode ProLine 21 system outputs Terrain Mode annunciation it does not use Annunciation EGPWS ASCII message DISPLAY BUS 1 CONNECT TO 453TX_1 A J1 58 Terrain Display data to Primary Flight Display Multi Function Display 1 B J1 59 DISPLAY BUS 2 CONNECT TO 453TX 2 A 1 56 Terrain Display data to Primary Flight Display Multi Function Display 2 1 57 Display Input Control Group 254 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429RX_1 Format ARINC 429 High Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms J2 36 Range Mode Range Word 6 2 21 176 Discrete 5 640NM Basic N A 50 C
251. ation Defined DC Inputs 4 2 4 AC Analog Inputs 4 2 4 1 Synchro Roll Attitude 4 24 2 Synchro Magnetic Heading 4243 Synchro Pitch Attitude 4 2 44 Configuration Defined Synchro Inputs 4 2 4 5 Signal Timing Reference Inputs 4 2 5 ARINC 429 575 Digital Serial Bus Inputs 4 2 6 RS 232 RS 422 Digital Serial Bus Inputs 4 2 6 1 GPS RS 232 Digital Serial Bus serial port 3 42 62 GPS RS 422 Digital Serial Bus serial port 3 4 2 6 3 Air Data RS 232 Digital Serial Bus serial port 2 4 2 6 4 Air Data RS 422 Digital Serial Bus serial port 2 4 26 5 SCI Range RS 422 Digital Serial Bus serial port 1 4 2 7 Discrete Inputs 4 2 8 Configuration Module Interface 4 2 9 GPS Antenna Input 4 2 10 OAT Voltage Reference Output 4 2 11 Lamp Driver Outputs 4 2 11 1 Monitor Output Characteristics 4 2 11 2 Discrete Output Characteristics 4 2 12 Audio Outputs 4 2 12 1 High Level Speaker Audio Output 4 2 12 2 Low Level Interphone Audio Output 4 2 13 ARINC Digital Serial Output Buses 4 2 13 1 ARINC 429 Output Bus 4 2 13 2 ARINC 453 Output Bus Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV 159 159 159 172 SHEET 154 Honeywell MK VI MK VIII EGPWS Installation Design Guide 43 FRONT PANEL TEST INTERFACE 4 3 1 4 3 2 4 3 3 RS 232 Maintenance Port serial port 4 PCMCIA SmartCable Port GSE Present Discrete Input 4 4 FRONT PANEL STATUS INDICATORS 5 AIRCRAFT APPLICATION DATA 51 CONFI
252. av 4331 l HOVDMddV 4331 TOES mie ao 5 2 3 x N 108170 dWv 1 43315 HS 1418 1 1071909 3 A 2 57 vere ONISV 52 ux Lu yf 109170 2 549 355 es 2 5 al SIX SN9 335 SWNT a RS u A gt Ha I 52 22 7192 1 HS NOILISOd vi N 1DdNI QAO 2833 Es 2 5 1 I v ui Nao BAT d dh n Le 1010 z no asa 25 0 ND 132592 dW31 SIV 29 LNdNI 132993 5 9 2 5 1 gt m erg 2x IASI dI tt IND za 1092 5440 E 1531 473 3L 3755 3 H 10114 d AD a p a Ariy Tay 192 gt ON AL f 30800 t dW 7 ND z WJ 827 1 SAdD NI C minam viva aIv SSN S3INDIAV 2 UN SNOILONNA 20 82 l3v8381v 313H9SId 18531 109100 1531 01 SHEET 143 DWG 060 4314 150 REV 7 Proprietary notice on title page applies SCALE NONE SIZE A CAGE CODE 97896 Honeywell MK VI MK VIII EGPWS netallatien Design Guide Y 9 2 z 2 z lt 5 5 ul 2 e 2 5 Eg a A 2 g do IS i i gt L o z o gt lt u 2 a S u z o IOC Optiona
253. bels on its ARINC 429 data bus KCPB bus types use amp Warning Annunciations in same Window therefore during EGPWS Self Test the Fail lights will not remain on throughout the test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 217 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 235 Collins ProLine 4 Non Integrated Display Configuration Group Collins ProLine 4 EE Sweep Type Standard with 60 degree limit YV l Auto Pop Up 5 37 Peaks Mode Category 7 Options Select Group 1 Manual select Anytime Manual deselect Anytime Auto Range 914 SOS Moving Marker No Overlay Page s TERR or Peaks Elevations located on upper left side of Terrain f eus Display bus type ARINC 453 o DISPLAY BUS 1 CONNECT TO 453TX 1 A J1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 B J1 59 7 2 DISPLAY BUS 72 CONNECT TO 453TX 2 J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 J1 57 7 2 Display Input Control Group 244 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms 2 36 Range Mode Range Word 6 2 21 155 Discrete 5 640NM Basic N A 50
254. ble 5 3 13 x use only the one that matches the aircraft wiring either 28V or Ground 3 15 1 1 Glideslope Inhibit Discrete The Glideslope Inhibit discrete is used for Backcourse Inhibit of Mode 5 Glideslope Either the 28V J1 38 discrete or the ground J1 19 discrete may be used If Backcourse is not available these discretes may be left open Discrete Position Status Connector Pin Glideslope Inhibit 28 Inhibit 28V J1 38 Not Inhibit Gnd Open Glideslope Inhibit Gnd Inhibit Gnd J1 19 Not Inhibit 28V Open 3 15 1 2 Landing Flaps Discrete Landing Flap discrete is supplied by a Flap or Flap handle switch The active position 28V or GND indicates Not Landing Flaps or Flaps Up and should be connected to a contact that will indicate Flaps Up until the Flaps are lowered to landing position prior to landing The Landing Flap discrete active position can be reversed by the Flap Reversal Option of Appendix E Table 5 3 7 as shown in the following tables Flap Override for MK Vill EGPWS can be done by a guarded or illuminated cockpit switch that simulates the Flap Down condition 28 VDC Landing Flap discrete active position Flap Reversal Category 7 Flap Discrete J1 37 False True Landing Flap discrete 28V Flaps Up Flaps Down Landing Flap Discrete Open or GND Flaps Down Flaps Cat 13 ID 254 255 only Flap Override OVRD 28V 28V Flap Override NORM Open Open
255. bstacle Caution or Warning alert event Pa ere WXR System R T WXR TERR 429Tx p 9242 pere 2 42911 453 OUT Displa A J2 37 429 Range 1 B 42 36 9 ARINC 429 RANGE BUS 9 Output Bus J2 41 Range 2 12 40 I 453 WX 453 1 x aes ARINC 453 TERRAIN BUS 1 E TERR EUS A J1 56 45382 J1 57 Spare 2 TERRAIN i E A POP UP Disereter 9151 Terrain Pop Up Discrete Output TERRAIN SELECTED 4 DSD 1 Gnd 121 32 Display Select DISPLAY RELAY Discrete 1 Input 28 VDC DSD 2 Gnd J1 31 Spare 2 Momenta Discrete J1 54 Terrain Display Select 1 Discrete Output Display relay specifications 4PDT Continuous Duty Cycle Pickup Voltage 13 5 Vdc Max Dropout Voltage 7 5 2 0 Vdc Coil Resistance nominal 500 Ohms 100 28 Vdc Coil Rating 26 0 nominal 34 Vdc max Contact V drop lt 125mV rated load Contact current rating 2 Amps resistive 28 Vdc EM6 disp vsd FIGURE 3 15 2 Example of Terrain Display Interface EGPWS J1 32 lt ism 7 A _ TERR DISPLAY 28V V EGPWS 28V J1 54 OFF ON D QD Amber Sed TerrDisSw vsd Figure 3 15 3 Example of Terrain Display switch with relay Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 112 Honeywell MK VI MK VIII EGPWS Installation Desi
256. chro 11 8 VAC Reference Dynamic Range Signal Dynamic Range 90 Synchro Angle 15 5 VAC max Signal Reasonable Range 80 Synchro Angle Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 272 Honeywell MK VI MK VIII EGPWS Installation Design Guide None External Validity Type one 6 1 9 Magnetic Heading 5 Wire Synchro The Magnetic Heading will be corrected with the internal Magnetic Variable Table External Validity Type Discrete Validity 28VDC 6 1 10 Uncorrected Barometric Altitude ADS 65 Signal Name Uncorrected Baro Altitude DC Voltage Signal Open Wire Threshold 3000 Feet 6 1 11 RT 221 300 Radio Altimeter Signal Name Radio Altitude RT 221 300 AIC Algorithm DC Absolute Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 273 Honeywell MK VI MK VIII EGPWS Installation Design Guide Discrete Validity 6 1 12 Pitch Synchro Attitude 3 Wire Synchro 11 8 VAC Signal Name Pitch Attitude 3 Wire Synchro AIC Algorithm 3 Wire Synchro 11 8 VAC Signal Dynamic Range 90 Synchro Angle 15 5 VAC max Signal Reasonable Range 80 Synchro Angle Signal Open Wire Threshold Reference Dynamic Range Input Reference Connection AIC Name S3 Synchro 3 External Validity Flag Connection J1 68 Common Validity with Roll Attitude 6 1 15
257. ciated with it Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 110 Honeywell MK VI MK VIII EGPWS Installation Design Guide TCAS TAS Connector Vendor Model Function PIN Honeywell CAS 81 TCAS Il TA Only RBP 5C TPA 81A Inhibit Audio RBP 5D Collins TTR 920 TCAS II TA Only RBP 5C Inhibit Audio RBP 5D CAS 66 67 Standby P1A 17 Inhibit Audio P1A 18 Goodrich Interface with the Goodrich Skywatch TAS Skywatch HP SKY899 P1 34 requires a 28V pullup resistor in the aircraft Skywatch SKY497 Inhibit Audio p1 32 wiring as shown in Figure 3 15 1 below TCAS TCAS791 A P1 9 n DIM TEST 11 34 elf Test Discrete Input PULLUP Z places aeg GPWS Warning Alert Discrete Output P TEST 11 15 5 Cancel Discrete Input Moneta GPWS J1 77 GPWS Caution Alert Discrete Output P I CANCEL J1 72 GPWS Inoperative Discrete Output J1 55 Terrain Not Available Discrete Output 11 12 errain Inhibit Discrete Input 1 76 Lee vanceled miscrete _________ J2 31 J1 52 Steep Approach Select Discrete Input lt 522 Steep Approach Select Discrete Output Guarded 1 1 Optional J1 14 22 __ _ 28V pullup Jiy3 ee software or later Flap Override Discrete Output lt gt 100K 2 om TCAS Audio On D
258. city labels ID s 10 13 and 253 are provided to support GPS interfaces that do not provide North South East West Velocity labels 166 amp 174 ID s 0 1 4 5 and 255 are preferred Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 63 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 5 4 ARINC 429 BUS Cat 3 ID 0 1 4 5 10 13 EGPWS MK VI MK VIII ARINC 429 GPS J2 CN ARINC 429 A 25 M ARINC 429 Bus Hi GPS Bus B ARINC 429 Bus Lo ARINC429 GPS vsd 429 GPS Alt ARINC Bus 1 Bus 2 Vendor Model Speed Ref 743 743A A B A B Collins GNLU 910A Notes High MSL 743A LMP 2J LMP 2K Collins GPS 4000 0 4 MSL 743A MP 11A MP 11B UNS GPS 1000 1 Low WGS 84 743 TP 12A TP 12B TP 11A TP 11B UNS GPS 1200 0 Low MSL 743A TP 12A TP 12B TP 11A TP 11B UNS 1C 1 Low WGS 84 743 1 P1 b 1017 3X XXX or 1017 4 UNS 1D 1 Low WGS 84 743 MP 10J MP 10K 1192 00 1111 or 1192 30 1111XX UNS 1F 1E 1L 0 Low MSL 743A MP 10J MP 10K MP 4J MP 4K 2192 00 11110X UNS 1K 1 Low WGS 84 743 MP 4C MP 4D 1116 3X 111X or 1116 4X 111X UNS 1M 1 Low WGS 84 743 P2 K P2 L 1013 4 GNS XLs 0 Low MSL 743A J101 N5 J101 N6 17960 0203 SM04 17960 0102 SM07 GNS XL 0 Low MSL 743A J101 N5 J101 N6 18355 SM06 GNS X
259. ckshell and contains electrically reprogrammable memory for configuration storage By this method the aircraft configuration is stored in the configuration module on the aircraft and each newly installed EGPWS computer does not require operator assisted programming before or during installation The aircraft configuration in the Configuration Module can be changed at any time by use of the WinVIEWS software as explained in Section 4 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 53 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 3 Category 1 Aircraft Mode Type Select Category 1 specifies the general aircraft type warning mode differences bank angle alert curve fixed or retractable gear and 3500 ft or 2000 ft min runway length as an option for MK VIII EGPWS only Appendix E Tables 5 2 and 5 3 1 include some information required by MK VI MK VIII EGPWS development personnel and not pertinent to the installation design process Only items relevant to the installation design process are discussed in this document 3 3 1 Aircraft Mode Type The Aircraft Type identifies the aircraft as GA Fast Turboprop GA Slow Turboprop or Bizjet Turbofan The aircraft category defines configurable airspeed limits for mode expansion and gear and flaps stuck down conditions reasonable test and also define the Mode 1 2 3 4 amp Bank Angle warning alert curve options
260. cleared when TERRAIN AWARENESS NOT AVAILABLE TERRAIN AWARENESS INOP are true 14 SPARE 19 SPARE 0 SPARE 21 SPARE SPARE SPARE 27 28 2 SPARE 11 12 13 14 15 16 17 18 19 2 21 22 23 24 25 26 27 28 29 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 310 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 3 3 Message Word 1 052 This label contains the color to be displayed on the 6 character terrain display window Label Octal 052 Transmit Interval 200 msec 10 E ee l 2 22 22 9 10 SDIQO Lon Spare 0 7 12 Spare 13 Spare 14 Spare 0 2222 15 Spare o O _7 Spare 18 j Spare 01 Spare 2 j sa o O 2 Spare 35 7 000 0001 Red Doge 000 0010 Amber 25 ChamcerCoor 0000011 Yellow 26 Character Color 0000100 Green 27 ChaacerCoor J 0000101 Cyan 28 Character Color 0000110 Magenta 0000111 White 7 1 3 4 Message Word 2 053 This label contains the first 2 characters to be displayed on the 6 character terrain display window l lx ee r 4 11 Spe 20 Gpc 0 0 12 Spr 1 31 1 13
261. cription in Section 4 4 2 Vendor Name Vendor P N Description QTY UM Honeywell P N Honeywell 704 2617 001 RS 232 Cable 1 EA X704 2617 001 1 8 3 Smart Cable The MK VI MK VIII EGPWS Smart Cable can be ordered using the following part numbers Vendor Name Vendor P N Description QTY UM Honeywell P N Honeywell 951 0386 001 Smart Cable 1 EA 951 0386 001 1 8 4 Terrain Database Cards The MK VI EGPWS Terrain Database Cards can be ordered using the following part numbers Vendor Name Vendor P N Description QTY UM Honeywell P N Honeywell 718 1391 xxx North amp South America 1 EA 718 1391 xxx Honeywell 718 1392 xxx Europe Africa Asia 1 EA 718 1392 xxx Honeywell 718 1393 xxx Asia Australia Pacific 1 EA 718 1393 xxx Honeywell 402 6075 xxx Label TDB Front Panel 1 EA 402 6075 1 8 5 Flight History Card The MK VI MK VIII EGPWS Flight History Card can be ordered using the following part numbers Vendor Name Vendor P N Description QTY UM Honeywell P N Honeywell 300 1151 006 Flight History Download 1 EA 300 1151 006 Honeywell 718 1593 001 Flight History Download 1 EA 718 1593 001 Note 1 Unprogrammed blank 32 Mb card ATA PCMCIA card Note 2 Programmed 32 Mb card ATA PCMCIA card 1 9 Accessorie s not Supplied 1 9 1 ARINC 453 Terrain Display wiring The Terrain display wiring ARINC 453 must meet the display manufacturer s specifications including termination method ARINC 453 bus wiring mus
262. d Fixed Gear aircraft Type 2 basic and Type 3 alternate Appendix E Table 5 3 5 defines the Audio Menu select options and identifies the first MK VI MK VIII EGPWS version in which the option was available see the Effectivity entry Appendix E Tables 5 3 5 x where X is the Audio Menu Type defines the voice callouts for each menu DGAC registered aircraft are required to use Alternate Audio Menu Recommendation Honeywell recommends the Basic Audio Menu except for DGAC registered aircraft 3 7 1 Audio Menu Selection Audio menu must be selected to provide EGPWS callouts The differences in the Audio Menu Types are shown in the following comparison tables ALERT WARNING Audio Menu CONDITION Basic Alternate Type 0 and 2 Type 1 and 3 Terrain Awareness Preface Terrain Terrain Terrain Ahead Obstacle Awareness Preface Obstacle Obstacle Obstacle Ahead Terrain Awareness Caution Caution Terrain Terrain Ahead Obstacle Awareness Caution Caution Obstacle Obstacle Ahead ALERT WARNING Audio Menu CONDITION Retractable Gear Fixed Gear Type 0 and 1 Type 2 and 3 Mode 4 Too Low Gear Too Low Flaps 3 7 2 Instructions Using Appendix E Tables 5 2 5 3 5 and 5 3 5 x as described above select the Audio Menu Type that matches the feature preferences and version part number being installed Basic or Alternate menu e Retractable Gear or Fixed Gear Record the ID number for the Audio Menu Type from Appendi
263. d by MK VIII EGPWS only provided that WS is included e on title page applies SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 305 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 1 3 Mode 6 Callouts Discrete 1 272 Data Label ignificant Bits Transmit Interval 100 msec 10 13 14 15 26 27 28 29 NOTE Bits 12 15 21 22 and 26 29 will be set to zero Not supported 20 21 22 3 4 5 2 2 2 7 1 1 4 Mode 6 Callouts Discrete 2 273 Data Label ignificant Bits ign Bit 100 msec 10 BIT NO 14 15 16 17 19 20 21 22 23 24 25 26 27 28 29 NOTE Bits 14 17 19 22 and 24 29 will be set to zero Not supported IJ B n z B 3 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 306 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 1 5 EGPWS Alert Discrete 2 274 14 _ 5 J WINDHEARWARNNG L 7 Q WINDHEARINOP 98 __ WINDSHEARCAUTION 492 D CALDUTSINPR O 22 40 JQ Q2Q VBBONBINOB C Za ENGINFAIINOP 1 2 TERRAIN AWARENESS WARNING OBSTACLE AWARENESS WARNING L IGa3 TERRAIN AWARENESS CAUTION OBSTACLE AWARENESS CAUTION
264. d in this ID Note 3 42 15 28V_DISC_13 Not Defined in this ID Note 3 i J1 50 MON_OUT_3 Output Not Defined in this ID Note 3 J1 52 DISC OUT 7 Output Not Defined in this ID Note 3 CENE Flashing Lamps GPWS Warning Discrete Flashing Yes J1 78 DISC OUT 1 Output Terrain Awareness Caution or Warning Flashing Yes Obstacle Awareness Caution or Warning Flashing Yes GPWS Alert Discrete Glideslope Only Flashing Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word bit if configured by the display type Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 263 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 5 Input Output Discrete Type 5 CHANNEL CONN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE coer Sac ns umm cgo mem Inr ose hs ad co pem See TAD INOP Discrete 41559 MONCOUT 2 Output Terrain Not Available DISC_OUT_3 Glideslope Cancel Discrete J1 73 DISC_OUT_4 Output Flap Override Discrete J1 69 DISC_OUT_5 Output Audio On Discrete J1 54 DISC_OUT_6 Output Terrain Display Se
265. e shown Appendix Table 5 3 8 x and are used to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 93 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 11 Category 9 Navigation Inputs Select Category 9 selects the Glideslope and Localizer Deviation interfaces and Glideslope Validity and ILS Tuned discretes Appendix E Table 5 3 9 defines the Category 9 Navigation Inputs Select options called Navigation Inputs Select Types and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry Appendix E Tables 5 3 9 x where x is the Navigation Inputs Select Type number define the format and electrical interfaces required to support each Navigation Input Select Type 3 11 1 Navigation Inputs Select Glideslope amp Localizer Inputs Glideslope Deviation is basic required and is available in analog and digital formats Localizer Deviation is an enhancement not required Note Numerous but not all Envelope Modulation cases require a localizer input Therefore a NAV ID that supplies both Glideslope and Localizer should be selected in this category if possible However due to hardware limitations use of localizer for installations that can only provide low level validity is not supported In these cases only ID 1 can be selected Envelope Modulation
266. e Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 206 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 8 Honeywell Bendix IN842A IN862A RDR 2100 RDS 84 86 Display Configuration Group 5 Display Type Bendix IN842A IN862A color radar display RDR 2100 and RDS 84 86 radar systems Sweep Type Sweep range 60 degrees Pop Up when display is in the Never Pop Up proper mode Peaks Mode Category 7 Options Select Group 1 5 Manual deselect Anytime Auto Range 914 Moving Marker Noce n Z s Overlay Page Yes TERR or Peaks Elevation located on upper right side of Terrain image Display bus type ARINC 453 el v 453TX 1 J1 59 7 2 Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True 3 7 453 2 A J1 56 Terrai
267. e Input A discrete input for test and Ground Support Equipment is provided Grounding this pin indicates to the EGPWS that test or Ground Support Equipment is connected to the computer Active Threshold Voltage Logic True lt 0 8 VDC Inactive Threshold Voltage Logic False gt 2 0 VDC Input Impedance gt 20 KQ Maximum Fault Current lt 500 HA Pin Assignment Signal Mnemonic J3 11 GSE_PRES 4 4 Front Panel Status Indicators The MK VI and MK VIII EGPWC front panel provides three LEDs for indicating system and LRU status A yellow LED labeled EXTERNAL FAULT is activated when a signal fault external to the MK VI or MK VIII EGPWC is detected A green LED labeled COMPUTER OK is activated when the MK VI or MK VIII EGPWC itself is okay A red LED labeled COMPUTER FAIL is activated when the MK VI or MK VIII EGPWC has detected an internal computer fault Refer to Product Specification 965 1180 601 for a detailed discussion of status indications recommended maintenance actions Self Test activation and response Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 173 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 AIRCRAFT APPLICATION DATA This section describes the MK VI and MK VIII EGPWS interfaces for aircraft applications Section 5 1 is a listing of the selection categories defining the various aircraft sensor interfaces and EGPWS functional opti
268. e affected by direct sunlight or exhaust gases from engines or heaters The probe tip should extend beyond the aircraft boundary layer into the turbulent airflow See manufacturer for specifications 2 3 9 OAT Sensor Installation Refer to manufacturer s procedures or applicable STC documentation 2 3 10 Cockpit Lig hts This section provides information for selecting locating and mounting of the MK VI and MK VIII EGPWS Cockpit lights NOTE The nomenclature given for each lamp is an example only Other manufacturers use nomenclature that is also acceptable Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 40 Honeywell MK VI MK VIII EGPWS Installation Design Guide NOTE All lights 1 Refer to Honeywell Product Specification 965 1176 601 for additional information and for electrical loads specification 2 All lights are 28 VDC dual bulb sun light readable non flashing 3 Inthe OFF condition all lights have dark background with visible nomenclature for action 4 If desired the lights may be put on a dimmer circuit for night operation 2 3 10 1 Description EGPWS alert warning Lamp Format 1 GPWS P TEST This assembly is illuminated with red background and activated during any Mode 1 through Mode 4 and Terrain Awareness alert or warning This assembly also includes a momentary switch that will activate EGPWS Self Test EGPWS warning Lamp Format 2 PULLU
269. e appropriate pins in the P2 connector 2 3 5 Configuration Module Installation The purpose of this procedure is to give an assembly sequence for assembly of the Configuration Module with the P2 connector and backshell A The P2 connector Honeywell part number 440 1233 001 vendor part number RD50F1OJVLC 15 when ordered comes with 50 contacts and a plastic backshell hood The Configuration Module will replace the Backshell Plate The Backshell Plate can be discarded Wire the Configuration Module to the P2 connector using contacts provided with the connector Wire per the following wire list Wire Color P2 pin Violet P2 17 Blue P2 16 Orange P2 33 Black P2 50 White P2 49 Red P2 32 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 31 Honeywell MK VI MK VIII EGPWS Installation Design Guide D Position Slide Lock and Spring Clip onto connector E Install Backshell Housing onto connector The Ground wire used for ESD discharge is terminated with shielded pigtails inside the backshell to the P2 connector F Organize and dress wire exiting from the backshell route Configuration Module wires in a coil Install Cable Clamp do not tighten Cable Clamp screws G Secure the Configuration Module to the connector using screws provided Tighten Cable Clamp screws as required CONFIGURATION MODULE ASSEMBLY REQUIRED Two items as follows 1 0 Connector P2
270. e display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGP WS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 204 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 6 Collins ProLine II 5x4 5x5 Display Configuration Group 3 Collins ProLine II 5x4 5 5 Sweep Type Standard with 60 degree limit 22 Auto Pop Up 587 Peaks Mode Category 7 Options Select Group 1 Manual select Anytime Manual deselect Anytime Auto Range 914 Moving Marker 904 SOS Overlay Page s TERR or Peaks Elevations located on upper left side of uus image Display bus type ARINC 453 o DISPLAY BUS 1 CONNECT TO 453TX 1 A J1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 _ MEE 20 42 NI DISPLAY BUS 72 CONNECT TO E l J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 Bun o Iu EE Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Form
271. e display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 Bendix PPI 4B with blue water capability required for Peaks display Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 213 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 15 Honeywell P880 660 440 Integrated WXPD with SCI range and A C symbol Display Configuration Group 13 Display Type Honeywell P880 660 440 radar displays Integrated with A C symbol Sweep Type Honeywell Peaks Mode Category 7 Options Select Group 71 5 3 7 Manual select Anytime 20 Manualdeselect_ Anytime Auto Range Moving Marker Yes across bottom ofdisplayy __ Overlay Page Yes for Peaks Elevations located lower left of the display Honeywell picture bus __ Display bus type Honeywell picture bus DISPLAY BUS 1 CONNECT TO 453TX_1 J1 59 7 2 453 2 pu E d Not supported for this display type Auto Pop Up Category 7 Options Select Group 1 5 3 7 Display Input Control Group 3 CHANNEL CONNECT TO SCI Bus 1 Fault Designation DISPLAY BUS 1 429 422RX 1 Format RS 422 12K baud Bus Basic A J2 36 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 37 Range Mode Range Word 6 5 1 1 80 4
272. e is a simple text file that should include each CVT Item used in this test procedure A sample command file for this test procedure is found on the following page The file must be a Text Only type of file such as those created in the Microsoft Windows NotePad program It should have a filename extension of CMD Once this file is loaded WinVIEWS can automatically display the current value of each parameter listed in the file Normal Operation for Ground Testing the EGPWS STEP 1 Connect the PC to the EGPWS via the RS 232 cable as defined above STEP 2 On the PC start Windows 3 1 or higher STEP 3 Start the WinVIEWS program STEP 4 Under the File Menu select the Load Command File option and load the appropriate Command File STEP 5 Use F6 to select Data Display Mode Each CVT Item listed in the Command File will be continuously updated at a rate of greater than once per second The values shown for the CVT Items listed will be the test values Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 147 Honeywell MK VI MK VIII EGPWS Installation Design Guide Command File MK68_GTP CMD The format for the WinVIEWS command file is 1 ASCII Text Only no spaces 2 ACVT Item as specified in the test procedure 3 Each Item Name is followed by a return or enter RawRA1 AnAtt1Val ARA1Val RawAACMHD DHDsc AACMHdVal RawBAIt1 RawIMHd1 RawBCAIt1 LandFIDsc
273. e selected configuration in a configuration module installed in the aircraft wiring physically part of one of the EGPWC mating connectors For example selecting Category 2 ID 1 defines the Air Data Input as ARINC 429 per Table 5 3 2 1 in Category 2 With this ID programmed into the configuration module the EGPWC will look for and use the interface defined for this ID Table 5 2 can be used to record the selected ID for each category for later reference when programming the configuration module This programming is accomplished using a programming software tool available from Honeywell or generating a data text string and transferring this data in either case via the EGPWC RS 232C see 4 3 1 to the configuration module Once programmed the configuration is available and read by any installed EGPWC on power up Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 174 Honeywell MK VI MK VIII EGPWS Installation Design Guide Selects a b Aircraft Type Mode Type Selects a Air Data Source Selects a Position Source Selects a Altitude Callouts Menu Selects a Audio Menu Selects a Terrain Display Config Selects a Steep Approach Enabled b TA amp D Alternate Pop Up c Peaks Mode Enable d Obstacle Awareness Enable e f Bank Angle Enable Flap Position Polarity GPS Altitude Reference Selects a Radio Alti
274. e that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Input Select from Appendix E Table 5 3 15 5 3 16 and 5 3 17 under the Ident No heading for Step Category 15 16 amp 17 in Appendix E Table 5 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 114 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION IV CONFIGURATION MODULE PROGRAMMING AND TERRAIN DATABASE LOADING Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 115 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION IV CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING SECTION IV CONFIG MODULE PROGRAMMING AND REGIONAL LOADINGCG 117 4 INTRODUGTION ree die eae E OR MAT ret ote to Ee e riae ota a aqu 117 4 2 HARNESS CHECKOUT AND POWER nne 117 43 UNIT INSTALLATION in aaa hy tete tan e D ate e Pere ram ata ap ete ee ee vei Rn 117 4 4 EGPWC INITIALIZATION AND 117 4 4 1 RS 232 Communication with the MK VI VIII EGPWS nn 117 4 4 2 EGPWC Front Panel Test Connector esee eee eene eene t
275. een TERRAIN on PFD and MFD by EFIS If Bit 13 or 22 1 then display red PULL UP on left and right PFD If Bit 12 or 23 1 then display amber GND PROX on left and right PFD If Bit 14 1 then display white GPWS FAIL message on PFD If Bit 15 1 then display red WIND SHR message on PFD If Bit 17 1 then display white WNDSHR FAIL message on PFD If Bit 18 1 then display amber WIND SHR message PFD If Bit 24 1 then display amber TERRAIN FAIL message on PFD and MFD Terrain window cleared by Epic If Bit 27 1 then display amber TERRAIN NA message on PFD MFD Terrain window cleared by Epic If Bit 28 1 and display configured for pop up on Pilots side then Pop Up Terrain on left MFD If Bit 29 1 and display configured for pop up on CoPilots side then Pop Up Terrain on right MFD If Bit 14 Bit 17 and Bit 24 1 then display amber EGPWS SYS FAIL on PFD in lieu of GPWS FAIL and WNDSHR FAIL messages on the PFD If bits 30 and 31 01 functional test then display white TERRAIN TEST on PFD and MFD Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 235 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 252 Honeywell SPZ8000 EDZ605 EDZ805 and EDZ806 with MK VIII Only ARINC 429 Range Display Configuration Group 250 Display Type Honeywell SPZ8000 new style
276. efore Timed Audio Inhibited Fault will be enunciated during cockpit Level 2 Self Test Level 6 Audio readout Timed Audio Inhibit Discrete Selected gt Timed Audio Inhibit Not Selected gt Timed Audio Not Inhibit 6 6 27 GPWS Inhibit Discrete This discrete inhibits all audio and visual except for Windshear Terrain Awareness and TCF Type Supplied by an alternate action latching and self indicating cockpit switch Signal Status GPWS enabled or disabled Fault monitoring Activation of this input for more than 5 seconds will result in the GP WS Inhibit fault which will cause a GPWS INOP indication Level 6 Audio readout GPWS Inhibit Discrete Selected gt GPWS Inhibit Not Selected gt GPWS Not Inhibit 6 6 28 Localizer Validity Discrete 1 A Localizer Validity discrete may be used by the EGPWS for localizer input from an ARINC 547 Nav Receiver Type Validity from ARINC 547 Nav Receiver Signal Status Valid or Invalid Level 6 Audio readout Localizer Validity Discrete 1 Valid gt Localizer 1 Valid Invalid gt Localizer 1 Invalid Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 302 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 OUTPUT DATA DEFINITION 7 1 ARINC 429 Output Data The MK VI and VIII EGPWC provides one or two ARINC 429 low or high speed output channels per section 5 3 6 3
277. eg Bus 2 A leg Bus 2 B leg 4 2 13 2 ARINC 453 Output Bus Quantity Format Data Rate Word Frame Structure Data definition Pin Assignment Signal Mnemonic Bus 1 A leg Bus 1 B leg Bus 2 A leg Bus 2 B leg 2 DITS ARINC 429 12 0 KBPS to 14 5 KBPS 100 KBPS 1 Type A broadcast for ARINC 429 Type B 32 bit words consisting of 8 bits label and 24 bits data status Refer to Section 7 12 43 429TX_1A 42 429TX 1B 12 26 429TX 2A 12 9 429TX 2B 2 1600 bit Manchester BI phase per ARINC 708A 1 Mb per second Refer to Section 7 2 Refer to Section 7 2 11 58 _1 11 59 1B 71 56 2 71 57 2 4 3 Front Panel Test Interface The MK VI and VIII EGP WS provide a 15 pin double density D Sub test connector on the front panel which provides interfaces for various test and maintenance functions This connector provides the following interfaces Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 172 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 3 1 RS 232 Maintenance Port serial port 4 One port is provided which meets the characteristics specified in RS232C This bus can be used to read internal data from the MK VI or MK VIII EGPWS for both bench and aircraft testing or transmitting configuration data for selected EGPWS interfaces and options Baud Rate 19 2
278. enet reet eene tnr eere een eere enn enne nns 118 443 WInVIEWS RE ene 119 4 AA WinVIEWS OpB6FPAtioh etaed lee dette 119 4 5 CONFIGURATION MODULE 2 119 43 4 CUM and CMR Comniands Les au a ed GRAN ERE REG 121 4 5 2 Configuration Module 122 4 6 TERRAIN DATABASE LOADING itte toto I RHETORIC EERE D EET RR PERIERE GE TR FIN 122 LOL Bfe i T 122 4 0 DIDVCSCHIPUON CE 123 60 2 Approval ee oe oar e cad eut 123 4 6 4 Material Cost and Availability eee eene 123 4 6 5 Accomplishment Instructions eee sese ttt tetit ettare t ESE SEENEN trente ertet erinnere 123 4 6 6 Verification of the Terrain Database Version 125 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 116 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION IV Config Module Programming And Regional Loading 4 1 Introduction The following procedures outline the steps necessary to accomplish a complete configuration of the MK VI MK VIII EGPWS This section must be accomplished in the order presented to minimize errors in configuring and
279. er Elevation 011 Transmit Interval 500 msec 10 ro ucc BIT DEFINITION Pno LAC o a Ta 9 50 0 Not Used 1 Captain uud F O Not Used s ng M g NR COLOR BIT 1 COLOR BIT 3 BLANK PEAKS i Normal Do PEE DASH PEAKS ELEVATION DISPLAY 0 Normal Display 1 Display Dashes SPARE 16 SPARE 19 SPARE NOTE Elevation bits are additive e g bits 20 amp 21 1 indicates 300 Ft Upper Peaks Elevation 1 51200 Ft 0 Failure 1 No Computed N Functional Test 1 Normal 0 Warning 0 Data 1 Operation 32 PARITY Odd Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 314 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 6 2 Peaks Lower Elevation 012 Data See Below Label Octal 012 Transmit Interval 500 msec 10 BIT NO DEFINITION COLOR BIT 1 12 2 Black o Green Yellow Magenta Blue White COLOR BIT 3 ET Digi 1 Display Dashes SPARE SPARE SPARE 19 SPARE NOTE Elevation bits are additive e g bits 20 amp 21 1 indicates 300 Ft Lower Peaks Elevation SIGN 0 0 Plus 1 51200 Ft SSM 0 Failure 1 No Computed Functional Test 1 Normal SSM 0 Warning 0 Data 1 Operation PARITY Odd 7 2 ARINC 708A Output Two channels of ARINC 708A or KCPB 453 data is provided to drive terrain displays for installations that use the T
280. erence the GPS position uses and set the GPS Altitude Reference accordingly in this Category Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 89 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 9 8 Instructions Review the sections above for information on Steep Approach TA amp D Pop Up Peaks Mode Obstacle Awareness Bank Angle Flap Reversal and GPS Altitude Reference Using Appendix E Tables 5 2 and 5 3 7 as described above select the preferred Category 7 Options Select Group 1 ID that matches the aircraft configuration features preferences and version part number being installed Record the ID number for the Options Select Group 1 from Appendix E Table 5 3 7 under the Ident No heading for Step Category 7 in Appendix E Table 5 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 90 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 10 Category 8 Radio Altitude Input Select Category 8 defines the Radio Altitude and Decision Height interface 3 10 1 Radio Altitude Input Appendix E Table 5 3 8 defines the Radio Altitude Types and identifies the first MK VI MK VIII EGPWS version in which the option was available see Effectivity entry Appendix E Tables 5 3 8 x where x is the Radio Altitude Type number define the format and electrical interfaces required to support each
281. errain Awareness display function Refer to document 060 4303 000 EGP WS Interface Methodology for further KCPB information See Category 6 for more details on individual displays 7 3 Audio Output Mode computation outputs generally result in an audio voice alert unless inputs are invalid or one of the audio suppression discretes is active The actual output message or intended message during audio suppression is sent to the alert lamp logic for proper output activation The audio outputs consist of an 8 ohm amplifier and a transformer isolated 600 ohm output Additional automatic volume control lowers both outputs a fixed 6 dB below the nominal level on command Refer to section 4 2 12 and Category 14 for information on volume levels Selectable sets of voice alert messages can be defined Each set is selected by the Voice Menu option in Category 5 7 4 Discrete Outputs Outputs from the various alert mode computations are first processed to determine which lamp outputs to produce All of the lamp outputs are driven by solid state switches to ground These outputs can also be used as discrete drivers for other devices All monitor lamp outputs are normally a steady state switch to ground Various formats of discrete outputs can be provided as defined in Category 13 7 4 1 Ground Proximity Alerts Discrete Lamp Outputs Two Lamp formats are defined as a function of the selected I O Discrete Type of section 5 3 13 For Lamp Format type 1
282. ette 122 4 0 2 DeS CHID OT tasqa tote ERE ere E E eee a 123 CN Inani EE 123 4 6 4 Material Cost and Availability 123 4 6 5 Accomplishment Instructions 123 4 6 6 Verification of the Terrain Database Version esee entere e nes 125 SECTION SCERTIBIGATION 5 USA Ou nsa Eee tovo E eset hos 128 S L INTRODUCTIONS rese deste tarte uw a ete ade reete diee Sama ha ELLE De sashes 128 5 2 CERTIFICATION PROCEDURE L rp UR ERE UOTE rp EHE E pe t RE ERSTER eSI 128 3 2 T Eguipment Compatibility nno dente aa aaa uut nepos iuquit 128 34 2 Bquipment Focdtion i nd oie ei edt eei eoa iR 128 2 2 3 FAA Requifemehts 128 3 2 4 Ground Test noa RES ere eld ERES 128 3 215 Flight Manual Revision susan e Ret ae dt Neid 128 SX MIT MEA 128 2 2 ee RUNI UU 129 5 2 8 Failure Modes Effects and Safety Analysis 129 SECTION VI MK VI GPWS TO MK EGPWS SIGNAL MAPPING 131 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 9 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX A
283. eversal and GPS Altitude Reference Appendix E Table 5 3 7 defines the Options Select group and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry 3 9 1 Steep Approach This feature desensitizes the Mode 1 Excessive Descent Rate alert boundaries to permit safe but steeper than normal instrument precision approaches e g MLS or GPS approaches without unwanted Mode 1 alerts Category 7 enables Steep Approach mode Category 13 Steep Approach discrete J2 31 cockpit switch activates deactivates the Steep Approach function during flight 3 9 2 TA amp D Alternate Pop up The Display Configuration Group Type Category 6 defines default and alternate definitions for EGPWS alert Pop up behavior when no terrain displays are active or when a combination of terrain and non terrain displays are active Some Display Configuration Group Types do not support an Alternate Pop up definition See Appendix E 5 3 6 1 X for definitions Category 7 enables disables TA amp D Alternate Pop Up 3 9 3 Peaks Mode Peaks mode is an alternate means of displaying terrain data The standard terrain display mode displays terrain relative to the aircraft altitude that is within the aircraft envelope the terrain is above or not more than 2000 feet below the aircraft The standard terrain display mode is typically blank during the cruise portion of a flight Peaks mode provides increased situational awarene
284. eviation of vertical position 6 4 3 Xpress GPS Packets ID 17 Ground Speed Track Angle O ValidFlag Valid 1 Invalid 0 Ground Speed Meters Second Track Angle Degrees 0 360 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 293 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 4 4 Xpress GPS Packets ID 18 East North Up Velocit O ValidFlag __ Valid 1 Invalid 0 East Velocity Meters Second North Velocity Meters Second Up Velocity Meters Second 6 4 5 Xpress GPS Packets ID 1C GPS State This packet contains information concerning the current state of the receiver subsystem O State Byte Dicee Tre 1 False Q re 4 Altitude AidingInUse Bye True l Fale 0 5 ______ Nav _____________ Byte _ Diserete tth ________ State binary 00 initialization 01 search the sky 02 acquisition 03 transition 04 navigation 05 navigation with possible data collection 06 navigation with position degradation 07 dead reckoning Integrity State true if set false otherwise 0 HDOP gt 4 0 Set in approach mode when RAIM is not available and the computed HDOP exceeds 4 0 1 RAIM unavailable Set when RAIM is not available in the current navigation mode integrity warning Set when a RAIM error is detected 3 RAIM unavailable masked Set when RAIM is not available in the current navigati
285. firm your installation Category 2 ID 5 1 6 or 13 depending on availability of labels 204 and 212 ID 5 is the preferred selection then ID s 1 6 and 13 in order of preference CIC air data computers installed without Baro Set pots should be configured as Cat 2 ID 1 EGPWS installations with the B amp D 2600 ADC should be configured for Cat 2 ID 6 because the B amp D 2600 Altitude Rate ARINC 429 label 212 has a poor response to altitude changes and causes nuisance alerts Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 59 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 4 3 Digital ARINC 575 Cat 2 ID 2 Air Data Type 2 ADC 80 or equivalent is a low speed digital ARINC 575 signal having the air data labels 203 206 212 and 213 EGPWS MK VI MK VIII J2 ARINC 575 Air Data oN oN AirDataBus 51 56 ARINC 575 Bus Lo bu QW ARINC575 ADC vsd Cat 2 Bus 1 Bus 2 Vendor Model ID A B A B Collins ADC 80 2 P3 35 P3 36 Collins ADC 82A B amp D 90004 2 J1 27 J1 9 NOTE contact the manufacturer s customer service to confirm your installation Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please SHEET 60 Honeywell MK VI
286. geometric altitude with the closest runway field elevation The callout may be optionally chosen to annunciate Five Hundred or Five Hundred Above This requires Category 6 ID other than 2 TAD TCF must be active Minimums Minimums callout be selected or deselected from these combinations by connecting or not connecting the Decision Height DH discrete J1 33 of Category 8 Recommendation Honeywell recommends at least a Smart 500 callout and Minimums Minimums callout FAA and JAA approved installations require a 500 foot callout Using Appendix E Table 5 2 and 5 3 4 as described above select the preferred Altitude Callout Menu Type ID that matches the feature preferences and version part number being installed Record the ID number for the Altitude Callout Menu Type from Appendix E Table 5 3 4 under the Ident No heading for Step Category 4 in Appendix E Table 5 2 If the Minimums Minimums callout will be used use the electrical interfaces pin outs for Radio Altitude Input Select Type Category 8 shown in Appendix E Table 5 3 8 x to generate the installation wiring diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 67 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 7 Category 5 Audio Menu Select Category 5 defines four Audio Menu options Retractable Gear aircraft Type 0 basic and Type 1 alternate an
287. gn Guide 3 15 3 Instructions Using Appendix E Tables 5 2 5 3 13 and 5 3 13 x as described above select the Input Output Discrete Type number that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Input Output Discrete Select number from Appendix E Table 5 3 13 under the Ident No heading for Step Category 13 in Appendix E Table 5 2 Using the Input Output Discrete Type number from Appendix E Table 5 3 13 as x go the Appendix E Table 5 3 13 The electrical interfaces for the Input Output Discrete Type are shown in Appendix E Table 5 3 13 and are used to generate the installation wiring diagrams Note When there are two discrete pin choices for the same pin function in Appendix E Table 5 3 13 use only the one that matches the aircraft wiring use only the 28V and OV or the Ground and Open definitions 3 16 Category 14 Audio Output Level Category 14 controls the Audio Output level for alert menu callouts cautions and warnings Refer to Category 13 for information on the Mode 6 Low Volume discrete Appendix E Table 5 3 14 defines the Audio Output Level options and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry The Nominal Volume Select is equivalent to MK VI classic MAX volume level The through 24 dB are successively lower volume from Nominal The Nominal outp
288. h Speed Bus Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 37 Left Angle of Attack Body 6 2 44 224 12 180 degrees Basic 0 0439453125 deg 100 B J2 36 Normal Angle of Attack 6 2 52 236 15 0101 0 00003051757812 80 CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms Right Angle of Attack Body 6 2 45 225 12 180 degrees Basic 0 0439453125 deg 100 Normal Angle of Attack 6 2 52 236 15 0101 0 00003051757812 80 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 257 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 13 Category 13 Input Output Discrete Type Select The following table provides identification of the Input Output Discrete Type Each entry in the Input Output Discrete Type column has a corresponding table that provides detailed information on the configuration For example the details for Input Output Discrete Type 0 are found in Table 5 3 13 0 Table 5 3 13 Input Output Discrete Type Select Input Output Software EGPWS Discrete Type P Effectivity Effectivity Table 5 3 13 x MKVIII Input Output discrete definitions 020 Lamp format 1 Input Output discrete definitions Input Output discrete definitions 2 Lamp f
289. have software level 01 14 Note 7 Requires Bendix Honeywell 80 series radar 1 e RDS 86 Note 8 ID 10 243 and 244 must have Category 7 Peaks Mode Enabled option selected Note 9 KCPB Digital Discrete Word supports softkey discretes for Flap Desense Steep Approach Glideslope Cancel and Self Test In this category the following signals are configured by the ID number Signal Name Signal Type Defined By Terrain Display Bus KCPB or ARINC Display Configuration Group ARINC 429 or RS 422 Display Input Control Group TA amp D Alternate Pop Up Defined directly in Table KCPB is also known as AlliedSignal Picture Bus ASPB Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 199 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 0 KC Picture Bus Display Configuration Group 0 Display Type KC PictureBus KCPBY 2 Sweep Type Curtain Vertical or Horizontal scan 0 O Auto Pop Up 527 Peaks Mode Category 7 Options Select Group 1 5 3 7 Elevations via overlay Manual select None Display controls selection O Manual deselect 7 None Display controls selection 0 y O Auto Range Controlled by display response if selected 10 NM range willbeused Moving Marker Overlay Page Controlled by display Display bus type KCPB 52377 24 e 453TX_1 B J1 59 72 Bee CEN EUN 453TX 2 B J1 57 72 Display Input
290. he EGPWS Terrain Display has been selected for the associated display The TERR DISPLAY annunciator also has a momentary switch that is used to manually select the Terrain Display The TERR INHIBIT annunciator provides visual indication that the EGPWS Terrain functions have been inhibited The TERR INHIBIT annunciator also has a alternate action switch that is used to manually inhibit the Terrain functions The GPWS FAIL TERR FAIL annunciator provides visual indication that the EGPWS GPWS modes or TA amp D and TCF modes have a disabled function Vendor Name Vendor P N Description QTY UM STACO 61406 001 TERRAIN DISPLAY ON 1 EA STACO 61406 002 TERR INHIBIT ON 1 EA STACO 61406 011 GPWS FAIL TERRAIN FAIL 1 EA 1 9 5 Cockpit Speakers The MK VI MK VIII EGPWS can interface to an 8 ohm audio speaker for cockpit annunciation of aural alerts Vendor Name Vendor P N Description QTY UM Quam 30 0578 Audio Speaker 1 EA Utah SP 3A Audio Speaker 1 EA 1 9 6 Temperature Probes The MK VI MK VIII EGPWS may be optionally interfaced to a dedicated 500 ohm temperature probe meeting the specifications of ARINC 575 Section 3 8 The installer may want to discuss availability of a dual element probe compatible with the EGPWS and with other systems on the aircraft with the manufacturers Vendor Name Vendor P N Description QTY UM CIC 05257 Single element unheated 1 EA Norwich 103 00157 3 Single element unheated 1 EA Nor
291. his input continuously for more than 60 seconds will result in the Self Test Invalid fault which will cause a GPW INOP indication Note This input is used to start and stop the Level 6 self test there is no audio output for this discrete in Level 6 6 6 8 GND ILS Tuned Discrete 1 Type Supplied by ILS VOR Mode Selector Signal Status ILS tuned or VOR tuned Level 6 Audio readout ILS Tuned gt ILS 1 Tuned GND ILS Tuned Discrete 1 ILS Not Tuned gt ILS 1 Not Tuned Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 298 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 6 9 28V ILS Tuned Discrete 1 Type Supplied by ILS VOR Mode Selector Signal Status ILS tuned or VOR tuned Level 6 Audio readout ILS Tuned gt 28 Volts ILS 1 Tuned 28 V ILS Tuned Discrete 1 ILS Not Tuned gt 28 Volts ILS 1 Not Tuned 6 6 10 Glideslope Validity Discrete 1 A Glideslope Validity Discrete may be used by EGPWS for the ARINC 547 Glideslope Receiver input Type Validity from ARINC 547 Glideslope receiver Signal Status Valid or Invalid Note Analog Glideslope monitoring requires that this input discrete or the Analog Low Level Glideslope Validity Discrete is always true whenever ILS is not tuned In other words that the flag is biased out of view Level 6 Audio readout Valid gt Glideslope 1 Valid Glideslope Va
292. his prevents the EGPWS from reporting an external bus fault on the second channel 4 Software Level 14 required for integrated display and popup Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 209 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 11 Collins WXI 701 711 PPI with Auto Range Display Configuration Group 9 Display Type Collins 00202140 Sweep Type Sweep Type Fan Peaks Mode Category 7 Options Select Group 1 5 3 7 Manual select Anytime 2 Manual deselect Anytime 2 Auto Range 1 Moving Marker _ Overlay Page Without Peaks TERR located at the bottom left of display With Peaks Peaks numbers located at the bottom left of display Display bus type ARINC 453 DISPLAY BUS 1 CONNECT TO 453 1 1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 222 22 142 DISPLAY BUS 72 CONNECT TO NUMEN EE gt J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 Bon s 7 er Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARI
293. id mounting components near equipment operating with high pulse current or high power outputs such as radar and satellite communications equipment In general the equipment should be Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 29 Honeywell MK VI MK VIII EGPWS Installation Design Guide installed in a location convenient for operation inspection and maintenance and in an area free from excessive vibration heat and noise generating sources The MK VI and MK VIII EGPWS have an internal heater blanket therefore they can be mounted outside the heated area of the aircraft The computers have been qualified for operation up to 50 000 feet and 55 C using the heater blanket All mechanical installation drawings connector assembly diagrams interwiring diagrams and connector pin assignment tables referenced in this section are located at the end of Section of this manual Determine the mounting location for the system components following the guidelines below Prior to installing any equipment make a continuity check of all wires and cables associated with the system Then apply power and check for proper voltages at system connectors and then remove power before completing the installation To allow for inspection or repair of the wiring of the connector assembly itself sufficient lead length should be left so that EGPWS may be moved several inches A bend should be made i
294. ied to the Mode 1 curves If Steep Approach is enabled Category 7 and the Steep Approach discrete is selected Category 13 then fixed positive biases are added to both the Sinkrate curve 500 fpm and the Pull Up curve 200 fpm Category 7 enables the Steep Approach function for the installation Steep Approach is activated using the Steep Approach discrete Steep Approach discrete 2 is selected in flight when starting a steep approach Steep Approach discrete 2 should not be hardwired On ground self test is inhibited if Steep Approach is active Momentary action Category 13 ID s 6 and 7 only Discrete Position Status Connector Pin Steep Approach Steep Approach Toggle Gnd J2 31 Normal no action Open Alternate action Category 13 all ID s except ID 6 and 7 Discrete Position Status Connector Pin Steep Approach Selected Gnd J2 31 Not Selected Open Momentary action preferred method enables a non latching cockpit switch Reference 3 15 2 9 Steep Approach Discrete for associated lamp output The Steep Approach output lamp activates when the switch is pressed or when Envelope Modulation automatically activates steep approach and deactivates on landing 3 15 1 12 GPWS INHIBIT Discrete alternate action The GPWS INHIBIT discrete inhibits the GPWS modes of the MK VI VIII EGPWS all audio and visual except for WS TA amp TCF This discrete is typically connected to an al
295. igital A RING 429 Cat 2 ID 5 1 6 13 s siete reete ete 59 3 4 3 Digital ARINC 273 Cat 24D 2 d te i e a d eed an iniu 60 3 4 4S hadin 2000 Cat 2 ID ette e e ee eee ge t eie ee Np al er etes 61 3 4 5 Digital ARINC 429 Dual IOC Buses Cat 2 ID 255 sss ener nennen nns 62 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 6 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 4 OANSTHUCTIONS 5 62 3 5 CATEGORY 3 POSITION INPUT SELECT 63 S ARINCGO723 Formatu acus uec bards Cou ces Sua tee k ha Cau iu Ga 63 3 5 2 GPS Altitude Label 076 63 3 5 3 North South East West ener trennen enne eren 63 3 5 4 ARINC 429 BUS Cat 3 ID 0 1 4 5 10 13 64 3 5 5 RS 232 Transmit Receive 9600 baud Cat 3 ID 3 22 2 22 2 0000 00000 65 3 5 6 Dual ARINC 429 BUS Cat 3 1D 253 amp 255 li eem i edet a re t eerie 66 S S ie e c e RI TO dete editi e etus 66 3 6 CATEGORY 4 ALTITUDE 5 2 rei i AS i e a n nennen eren en rennen E nnne eren 67 3 7 CATEGORY AUDIO MENU SELECT Suasana tte bob Gee rte cecinisse
296. ignal having the air data labels 203 206 212 and 213 Air Data Type 5 is a low speed digital ARINC 429 signal having the air data labels 203 204 206 212 and 213 Air Data Type 6 is a low speed digital ARINC 429 signal having the air data labels 203 206 and 213 Air Data Type 13 is a low speed digital ARINC 429 signal having the air data label 203 only If the hardware is capable of transmitting all label sets the preferred Air Data Type is 5 If only label 204 is missing use Air Data Type 1 and if both labels 204 and 212 are missing use Air Data Type 6 Some aircraft have only label 203 available or no temperature for those choose Air Data Type 13 EGPWS MK VI MK VIII J2 ARINC 429 Air Data ARINC 429 Low Speed ARINC 429 Bus Hi Bus B ARINC 429 Bus Lo Digital ADC vsd Cat 2 Bus 1 Bus 2 Vendor Model ID A B A B Honeywell AZ 6XX 5 J1B 26 J1B 27 J1B 70 J1B 71 AZ 8XX CIC 04471 5 J1 12 J1 13 CIC 02702 mod 6 J2 J J2 K KDC 281 2811 5 2811 6 KDC 481 P4811 U 4811 1 B amp D 90004 5 J1 27 J1 9 B amp D 2600 6 6 8 B amp D 2601 14 13 B amp D 2800 201 11 201 28 Collins ADC 85 86 5 2 9 2 10 2 29 2 30 Shadin ADC 2000 5 J1 40 1 22 s w mod 71 73 01 NOTE connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to con
297. igure of Merit HSID Hardware Software Interface Document IO Input Output IAC Integrated Avionics Computer ICD Interface Control Document ILS Instrument Landing System INOP Inoperative IOC Input Output Concentrator IRS Inertial Reference System ISO International Standards Organization IVS Inertial Vertical Speed KT Knots KTS Knots LED Light Emitting Diode LRRA Low Range Radio Altimeter LRU Line Replaceable Unit LSB Least Significant Bit LT Less Than MCP Mode Control Panel MDA Minimum Barometric Altitude MFD Multi Functional Display MKII Mark Two Warning Computer MKV Mark Five Warning Computer MKVI Mark Six Warning Computer MKVII Mark Seven Warning Computer MKVIII Mark Eight Warning Computer MLS Microwave Landing System MMU Memory Management Unit MSB Most Significant Bit MSL Mean Sea Level N A Not Applicable NCD No Computed Data ND Navigation Display NVM Non Volatile Memory OMS Onboard Maintenance System P N Part Number PAR Parity PC Personal Computer PCMCIA Personal Computer Memory Card Industry Association PFD Primary Flight Display Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 325 Honeywell MK VI MK VIII EGPWS Installation Design Guide Acronym Interpretation PMAT Portable Maintanence Access Terminal PP Program Pin PVM Processor Voice Memory PWS Predictive Windshear System QFE Corrected Baro Alt relative to field elevation
298. in on the Left J1 Right J2 and Upper J3 connectors and provides a place for recording the actual usage for this installation 3 2 1 Primary Power Input The MK VI VIII EGPWC requires a primary power input 28 VDC input power and ground The Primary power should be connected as follows for the MK VI VIII EGPWC J1 40 J1 60 28 VDC Input J1 41 J1 61 are internally J1 41 J1 61 28 VDC Return shorted to each other Recommended EGPWC Power Control Device 3 Amp Delayed Action Circuit Breaker Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 51 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 2 2 Chassis Ground Chassis ground provides a redundant metal connection and should not be used as a normal current carrying conductor Chassis ground should be connected as follows J1 42 J1 53 GND Pins J1 42 and J1 53 are both connected to chassis ground internally It is not necessary to tie them both to ground in the aircraft wiring Pin J1 53 was made available to provide a convenient way to supply a ground to external equipment If the OAT probe is not present nothing needs to be tied to J1 53 3 2 3 GPS Antenna GPS antenna connector is available on the front of the MK VI EGPWS 965 1190 0XX MK VIII EGPWS 965 1220 0XX See Appendix E paragraphs 3 2 2 and 4 2 9 for connector details The J1 connector backshell supplied with classic MK VI GPWS instal
299. ion 352m Flaps Up Landing Gear Down Landing Gear Up Notes Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 140 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX Sample Wiring Diagrams Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 141 Honeywell MK VI MK VIII EGPWS Installation Design Guide V 19 380914 SAdD 33NHN3 WYSOVIC ll wX uoH 100 735 Neil VIVI 118 304 al MOLVASN3D IDAWAS 178 J3NVd LNAWNALSNI 10714 07 13388 Xog MOV TANVd LNAWNYLSNI 1071909 d 97192 123738 NIV8831 91 904 J 17 112 41450 1714 5214 Z dAL NI XA I XA E ANY OL JAA NNOL38 TWNDIS 2 ON aer ino 135 sa3i He 9190 118 30 E m MDIVN3N3O TUSWAS 17 P 09 123138 bri 18 20 112 1450 17802 LE 2 LUN 00 9355 131932030 STSSVHO RO vl 192
300. ion is controlled by display Manual deselect ________ Deselection is controlled by display o y O Auto Range Yes 10 controlled by display O Moving Marker Overlay Page Yes TERR or Peaks Elevations located on upper left side of Terrain image Peaks does not support sea level blue water Display Priority Standard Display bus type ARINC compatible format Collins ProLine 4 label 077 Terrain Mode Annunciation Standard DISPLAY BUS 1 CONNECT TO 453 1 1 58 Terrain Display data to switching relay Symbol Generator B J1 59 DISPLAY BUS 2 CONNECT TO 453TX 2 J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 J1 57 7 2 Display Input Control Group 244 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429 422RX 1 Format ARINC 429 High Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms 2 36 Range Mode Range Word 6 2 21 155 Discrete 5 640NM Basic N A 50 CHANNEL CONNECT TO IOC 2 Bus Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic Auto Pop Up Category 7 Options Select Group 1 5 3 7 TAS amp D Alternate Pop Up False TA amp D Alternate Pop Up True 5 3 7 2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms 2 40 Range Mode Range Word 6 2 21 155 Discrete 5 640NM Basic N A 50 Out
301. ironments without crew intervention 1 5 6 Smart Cable PCMCIA Interface The EGPWS Smart Cable part number 951 0386 001 is a removable PCMCIA card interface The Smart Cable is compatible with Honeywell supplied ATA style PCMCIA cards for use with MK VI and MK VIII EGPWS The purpose of the Smart Cable in the EGPWS system is for upload of software and databases and also for download of EGPWS Flight History The Smart Cable loading operation will closely emulate that of an ARINC 615 Data Loader Reference Figure 1 1 MK VI MK VIII EGPWS SMART CABLE E POWER IN PROC GARD CHNG XFER COMP FER FAIL SMART CABLE PART NO 951 0386 USED WITH MK VI GROUND PROXIMITY WARNING SYSTEM 9 MOD STATUS 58 00 FIGURE 1 1 VIII EGPWS SMART CABLE Proprietary notice title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 17 Honeywell MK VI MK VIII EGPWS Installation Design Guide 1 6 Technical C haracteristics MK VI VIII EGPWS TSO Compliance Physical size HxWxD Weight Mounting Temperature operational Altitude range Cooling Shock Power Consumption 28 VDC MK TSO C92c TSO C151b Class A MK VIII TSO C92c TSO C151b Class TSO C117a Application for UKCAA
302. is not shown if Range Keys are requested on label 012 Key Press Display Mode 4 The Display group is configured by the Display using response labels on its ARINC 429 data bus 5 KCPB bus types use amp Warning Annunciations in same Window therefore during EGPWS Self Test the Fail lights will not remain on throughout the test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 200 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 1 No Display TAD and TCF enabled No Table Table 5 3 6 1 2 No Display TAD and TCF disabled No Table Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 201 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 3 Collins Pro Line 4x4 Display Configuration Group 6 Display Type Collins Pro Line H 4x4 Display O C Sweep Type Standard with 60 degree limit O C Auto Pop Up 5 3 7 Peaks Mode Category 7 Options Select Group 1 Elevations via overlay Manual select Anytime 0 Manualdeselect Anytime 20 Auto Range 117 MovingMarker G O Overlay Page Yes TERR located on the left side of display Peaks Elevations located on the upper left side of Terrain image Displaybustype ARINC433 17 DISPLAY BUS 1 CONNECT TO 453TX 1 A J1 58 Terrain Displa
303. iscrete Output Note All EGPWS Outputs are Ground active and are intended to operate Lamps2 vsd with a 28V lamp source or 28V pullup external to the EGPWS FIGURE 3 15 1 Example of Light switch Interface Lamp Format 2 3 15 2 11 Terrain Dis play Select 1 amp 2 Discrete Terrain Display Select 1 amp 2 discrete J1 54 amp J1 49 will activate after the related pilot has initiated manual selection of the Terrain Display Select momentary discrete 1 or 2 J1 32 amp J1 31 Category 6 This feature activates a TERR white lamp located in the cockpit within sight of each pilot The lamp serves to remind the flight crew that this function is active The select switches J1 32 amp J1 31 and the indicator lamps J1 54 amp J1 49 are commonly combined in switch lamp assemblies mounted near the displays being selected Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 111 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 15 2 12 Terrain Pop up Discrete Terrain Pop Up discrete J1 51 will activate when a Terrain Obstacle Caution or Warning alert event has occurred This feature activates the pop up in an integrated display or will switch a relay to pop up Terrain display over selected weather radar display The Pop Up discrete can be used by a display system to differentiate between a manual Terrain display selection or Terrain display selection due to a Terrain O
304. iscretes 271 Mode 6 Callouts Discrete 1 272 Mode 6 Callouts Discrete 2 273 EGPWS Alert Discrete 2 274 EGPWC Alert Discrete 3 300 Internal Data Outputs Geometric Altitude VFOM 135 Terrain Clearance 164 Geometric Altitude 261 Computed Terrain Clearance 067 Latitude Selected EGPWS 310 Longitude Selected EGPWS 311 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 157 7 1 2 7 7 1 2 8 7 1 2 9 Honeywell MK VI MK VIII EGPWS Installation Design Guide Body Angle of Attack Right 223 MK VIII EGP WS w Windshear only Body Angle of Attack Left 224 MK VIII EGP WS w Windshear only Corrected Airspeed 242 MK VIII EGPWS w Windshear only 7 1 2 10 Windshear Warning Threshold 331 MKVIII EGPWS w Windshear only 7 1 2 11 Corrected Longitudinal Acceleration 332 MKVIII EGPWS w Windshear only 7 1 2 12 Raw Total Shear 362 MKVIII EGPWS w Windshear only 7 1 2 13 Corrected Normal Acceleration 364 MKVIII EGPWS w Windshear only 7 1 2 14 Computed Flight Path Angle 375 MKVIII EGPWS w Windshear only 7 1 2 15 Scaled Total Shear 376 MKVIII EGPWS w Windshear only 7 1 3 7 1 3 1 7 1 3 2 7 1 3 3 7 1 3 4 7 1 3 5 7 1 3 6 7 1 4 7 1 4 1 7 1 5 7 1 5 1 7 1 5 2 7 1 5 3 7 1 6 7 1 6 1 7 1 6 2 Terrain Display Outputs Displayed Range 050 Terrain Display Status Word 051 Message Word 1 052 Message Word 2 053 Me
305. isted below PFD Mode Select Word BIT NO DEFINITION 19 20 MDA Display Selection Bit 19 MDA not selected X Not used DH Display Selection DH Not Selected sj DH Selected 0 1 0 selected Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 288 Honeywell MK VI MK VIII EGPWS Installation Design Guide Navigation data source currently displayed on the Primary Flight Display PFD The table below show decimal values with bit 25 the LSB Values currently used by EGPWC 00 Not Used 08 MLS 1 01 Not Used 09 MLS 2 02 VOR LOC 1 10 ILS 1 03 VOR LOC 2 11 2 ILS 2 04 FMS 1 12 1 05 FMS 2 13 1 06 5 3 14 Not Used 07 Not Used 15 Not Used NOTE 1 Code 12 and Code 13 are currently assigned to Data source Neither of these states used by the EGPWC to select or evaluate input data 6 2 48 FWC amp GP Discrete Word 171 DISCRETE WORD FWC amp GP Source FWC or GP 1 amp 2 LABEL Octal 171 Units N A Approx LSB N A Data Bits Discrete word see below Sign Bit N A Transmit Interval mSec 100 Data Type Discrete SDI Bits 9 10 See below Note Several formats exist for this label Format 1 is the default format Format 2 will be specified if required in the Display Input Control Group FWC or GP WORD BIT ASSIGNMENTS Format 1 DEFINITIO
306. it N A SDI Bits N A BITS 18 to 24 Display Range 5 to 640 NM Format as follows Bits 24 18 7 bits zero Bit 18 set Bit 19 set Bit 20 set 6 2 22 Hazard Range Output 077 Source Wx Radar Approx LSB N A N A SDI Bits N A HAZARD RANGE OUTPUT BIT ASSIGNMENTS DEFINITION 1 Event Number LSB Not Used by EGPWC 12 Event Number Not Used by EGPWC 14 Range Start 0 0625 NM Not Used by EGPWC 15 Range Start 0 125 NM Not Used by EGPWC 11 12 13 14 15 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 282 Honeywell MK VI MK VIII EGPWS Installation Design Guide BITS 28 amp 29 Alert Level format as follows BITS 30 amp 31 SSM as follows 0 0 0 jNormalOperation 1 0 Level Advisry _ 1 Invalid fault r O 17 Leve2 Cauion __ 0 Funciona Test 6 2 23 Range 050 Multifunction Signal Generator MG or IC600 RANGE MG LABEL Octal 050 Units N A Max Range N A Approx LSB N A Data Bits Discrete word containing both N A Sign Bit N A Pad Bits 9 10 left and right ranges see below Transmit Interval mSec 100 ms Data Type Discrete SDI Bits N A Note Data format identical to EPGWC output label 050 BITS 11 to 14 Left Terrain Display Range 0 5 to 2000NM Format as follows BITS 15 to 18 Right Terrain Display Range 0 5 to 200
307. it first an ODD parity bit and one stop bit high The most significant bit of the character is a label or data flag bit The data rate of the SCI bus is 12 KBS 0 01 Channel 429 422RX 1 J2 36 37 and 422RX 2 J2 10 11 can be configured for this input Only two of the words on the bus are decoded Label 80 Mode Range Word 1 and Label FF Status Word 1 6 5 1 1 Serial Control Interface SCI Mode Range Word 1 80 Mode Range Word 1 Source Map Electronics Unit MEU LABEL Hex 80 Units N A Max Range N A Approx LSB N A Data Bit 1 8 Sign Bit N A Pad Bits N A Transmit Interval mSec See above Data Type Discrete SDI Bits N A Note this is an RS 422 serial data stream not ARINC 429 so SDI and SSM for this word are not applicable Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 295 Honeywell MK VI MK VIII EGPWS Installation Design Guide DISPLAY RANGE BIT ASSIGNMENTS DISPLAY MODE BIT ASSIGNMENTS Bits 4 7 Display Mode Displayable Display Mode used for bolt on EDZ displays only 6 5 1 2 Serial Control Interface SCI Status Word 1 FF Status Word 1 LABEL Hex FF _ Units N A Data Bit 1 8 Sign Bit Transmit Interval mSec See above STATUS WORD BIT ASSIGNMENTS BIT DEFINITION 1 SECTOR SCAN 2 TARGET ENABLE 3 P 450 4 ERASE 5 VAR GAIN 6 SLAVE 7 RIGHT 8 0 Always zero in data word
308. it within sight of the pilots 3 15 2 4 TAD INOP Discrete The TAD INOP discrete J1 55 indicates Terrain Clearance Floor TCF Terrain Awareness TA and Terrain Display are Not Available This feature activates a TERRAIN NOT AVAILABLE lamp located in the cockpit within sight of the pilots 3 15 2 5 GPWS Warning Discrete Lamp Format Type 1 definition GPWS Warning discrete J1 78 will activate during any Mode 1 through Mode 4 alert or warning Terrain Awareness caution warning or Obstacle Awareness caution warning This feature activates a GPWS lamp located in the cockpit within sight of each pilot Note that Mode 6 does not activate any lamp outputs only voices Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 109 Honeywell MK VI MK VIII EGPWS Installation Design Guide Lamp Format Type 2 definition GPWS Warning discrete J1 78 will activate during any Mode 1 or 2 Pull Up warning Terrain Awareness warning or Obstacle Awareness warning This feature activates a GPWS lamp located in the cockpit within sight of each pilot 3 15 2 6 GPWS Alert Discrete Lamp Format Type 1 definition GPWS Alert discrete J1 77 will activate during Mode 5 Glideslope cautions only This feature activates a BELOW GS amber lamp located in the cockpit within sight of each pilot Lamp Format Type 2 definition GPWS Alert discrete J1 77 will activate during a
309. itary M22520 2 09 1 10 3 Insertion Removal Tool P1 P2 P3 Description UM QTY Vendor Name amp Part Number Removal Tool P1 P3 EA 1 Daniels DRK 95 22M Removal Tool P1 P3 EA 1 Military M81969 8 02 Removal Tool P2 EA 1 Daniels DRK145 Insertion Tool P1 P3 EA 1 Daniels DAK 95 22M Insertion Tool P1 P3 EA 1 Military M81969 8 01 Insertion Tool P2 EA 1 Daniels DAK145 Insertion Removal Tool P1 P3 EA 1 Military M81969 1 04 Insertion Removal Tool P2 EA 1 Military M81969 1 02 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 24 Honeywell MK VI MK VIII EGPWS Installation Design Guide 1 10 4 Spare Connectors and Contacts P1 P2 P3 P N Description UM QTY Vendor Name amp Part Number 440 1223 002 15 pin male with hood EA Positronic Ind DD15M10YOC 15 440 1223 003 15 pin female EA Positronic Ind DD15F1000C 15 440 1223 004 15 pin male EA Positronic Ind DD15M1000C 15 400 5163 002 15 pin clamp kit EA AMP 745854 3 male contacts for 15 pin 22 30 AWG EA Positronic Ind MC8022D male contacts for 15 pin 22 30 AWG EA M39029 58 360 Positronic Ind FC6020D M39029 63 368 Positronic Ind FC8022D M39029 57 354 female contacts for 50 pin 20 24 AWG EA female contacts for 50 pin 20 24 AWG EA female contacts for 78 pin 22 30 AWG EA female contacts for 78 pin 22 30 AWG EA Sh X c lll Ce These parts are available in EGPWS kit PN 755 7013 090
310. ith warning voice over 8 Q speaker 3 Watts with Internal GPS includes antenna power 49 Watts typical with heater blanket on Recommended Power Control Device 3 Amp delayed action circuit breaker Pin Assignment Signal Mnemonic 28 VDC Input J1 40 J1 60 PWR 28 VDC Return J1 41 J1 61 PWR L Based on the Honeywell GPS Pxpress card specification and applies to 965 1190 0XX and 965 1220 0XX only 2 The heater blanket turns on at temperatures lt 23 C and turns off at temperatures gt 20 Note that this is not a floating input 28 VDC must be applied to both PWR_H and 28 VDC Return to both PWR inputs Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 164 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 2 3 DC Analog Inputs Unless otherwise specified Input Signal accuracy is 1 linearity 0 1 full scale offset 4 2 3 1 Radio Altitude Quantity Input Impedance each leg Maximum Reverse Fault Current Signal Range Input Voltage Range Conversion Range Input Filter Broken Wire Detect Pin Assignment Signal Mnemonic Signal Return 4 2 3 2 Low Level Glideslope Quantity Input Impedance each leg Reverse Fault Current Signal Range Input Voltage Range Input Filter Input Type Common Mode Voltage Range Broken Wire Detect Pin Assignment Signal Mnemonic Up Below Beam Fly Up
311. its 14 to 28 15 Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 1000 Maximum Data Type 2 s Complement Binary SDI Bits 9 10 The VDOP scaling is multiplied by 16 to produce VFOM values required by the EGPWS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 279 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 2 16 Sensor Status 273 GPS SENSOR STATUS BIT ASSIGNMENTS DADS Status Present 0 Not Present 1 DADS Source Primary 0 Secondary 1 IRS FMS Status Present 0 Not Present 1 IRS FMS Source Primary 0 Secondary 1 Current System in Use 00 GPS 10 GLONASS 11 GPS GLONASS 01 Spare Operational Mode 000 Self Test Mode 001 Initialization Mode 010 Acquisition Mode 011 Navigation Mode 100 Altitude Clock Aiding Mode 101 Differential Mode 110 Direction Speed Aiding Mode 111 Fault DADS Input is NOT required if ALTITUDE Data to GPSSU Sensor is Received from IRS FMS Inputs 6 2 17 Universal Time Correlation 125 GPS UNIVERSAL TIME CORRELATION UTC BCD Source ARINC 743 A GPSSU LABEL Octal 125 Max Range See NOTE 1 Approx LSB 0 1 Minute Data Bits See NOTE 2 Sign Bit Pad Bits N A Transmit Interval mSec 1000 Maximum Data Type BCD SDI Bits 9 10 NOTE 1 Maximum value 23 59 9 NOTE 2 BCD BIT Assignments per Table be
312. ive the GPS input AGC circuitry and actually reduce performance The following GPS antennas are found to be compatible with the EGPWS internal GPS card Other GPS antennas may be found compatible contact EGPWS engineering for assistance It is the responsibility of the OEM or owner operator and ultimately the regulatory authorities to assess the antenna acceptance criteria relative to ARINC MIL or other specifications Boeing has certified the Sensor Systems antenna S67 1575 133 an ARINC 743A antenna with a 33dB gain for use on all A C This antenna is certified for HIRF EMI Class 1 flight critical operation As a result it is very expensive about 3X other versions King KA 92 P N 071 01553 0200 TSO C129 Sensor Systems P N 567 1575 52 TSO C129 ARINC 743A Sensor Systems P N 567 1575 133 TSO C129a ARINC 743A The EGPWS requires an input signal of no less than 106 dB at the EGPWS GPS coax connector Installers need to calculate signal strength plus antenna gain minus cable line loss to ensure that the input signal does not exceed the 106 dB limit To calculate signal strength at the EGPWS coax connector assume a received signal strength of 118 dB at the antenna this is average signal strength from a GPS satellite at zenith over the antenna Add the gain of the antenna then subtract the line loss of the coax cable and insertion loss at each connector except at the EGPWS Assume 0 6 insertion loss per connector EXAMPLE Active
313. l Interface for Input Output Concentrator AUTOPILOT ENGAGED GEAR SWITCH FLAP SWITCH Proprietary notice title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 144 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX C WinVIEWS OPERATION INSTRUCTIONS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 145 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX C WinVIEWS Operation Instructions RS 232 COMMUNICATION WITH THE EGPWS EGPWS contains software that allows monitoring of its internal parameters for testing purposes without altering its operation The monitoring of these parameter values enables the operator to quickly determine if the correct signal and scaling is being used by the EGPWS computer The communication link utilizes the RS 232 Communication Protocol configured as follows 19200 Baud No Parity 8 bits and 1 stop bit The RS 232 interface with the EGPWS is accomplished via the J3 test connector on the front of the EGPWS The connection between a PC with a standard DB9 serial port connector and the EGPWS RS 232 interface is defined as follows Please note that the EGPWS will activate its RS 232 port only when it receives the command CONTROL Z after power is applied to the EGPWS The CONTROL Z command is automatically sent by WinVIEWS RS 232 Receive RS 232 Transmit RS 232
314. l Speed and Altitude 2 4 5 253 gt ARINC 429 via dual IOC buses Note 1 hn MER 55 55 2 2 Digital Roll and Acceleration N ARINC 429 via dual IOC buses Note 1 Note 1 ID 253 and 255 may only be used in conjunction with other IOC bus selections for categories 2 6 8 9 11 and 12 Note 2 Category 10 and Category 11 use the same ARINC 429 receiver if a digital source is selected X Table 5 3 10 0 Attitude Input Select Type 0 SIGNAL SUMMARY DATA Format 3 Wire Synchro X 1 1 Input Type Basic Roll Attitude Y 1 21 6 1 8 Fault Designation ROLL FAULT 2 2 Validity None Reference None Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 252 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 10 2 Attitude Input Select Type 2 REFERENCE Format 3 Wire Synchro with Validity Flag X 11 1 Input Type Basic Roll Attitude 21 Fault Designation ROLL FAULT 2 J1 2 Validity Attitude Validity Discrete 1 Reference None Format 3 Wire Synchro with Validity Flag Input Type Basic Pitch Attitude Fault Designation PITCH FAULT Validity Attitude Validity Discrete 1 Reference None CONNECTION PIN TYPE CHANNEL DESIGNATION Polarity REFERENCE Configuration Discrete 1 lt 4 4 Invalid 4 2 7 Table 5 3 10 4 Attitude Input Select Type 4 SIGNAL CONNECTION Format 3 Wire Synchro with Validity Flag X
315. lack background with white legend Colors are per FAR 23 1322 GPWS system validity GPWS INOP This assembly is illuminated with amber background and activated during any detected partial or total failure of the GPWS modes 1 5 TERRAIN select TERR DISPLAY ON Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 41 Honeywell MK VI MK VIII EGPWS Installation Design Guide This assembly is illuminated with white background and activated after the flight crew has initiated the manual selection of the EGPWS terrain display for the associated cockpit display This assembly also includes a momentary switch that will activate EGPWS Terrain display feature TERRAIN inhibit TERR INHIBIT ON This assembly is illuminated with amber background and activated after the flight crew has initiated the manual inhibit of the EGPWS Terrain Awareness amp display and Terrain Clearance Floor functions during an approach to an airport not in the EGPWS Terrain Runway database This assembly also includes a alternate action switch that will inhibit EGPWS TA amp D and TCF functions TERRAIN system validity TERR FAIL This assembly is illuminated with amber background and activated during any detected partial or total failure of the TA amp D or TCF functions 2 3 10 2 Location Cockpit layout size and operator s preference will determine if only one set of lights is used i e mounted in the center or if
316. laps Discrete Gnd Flaps Up 118 2ND DISE 03 Flap Override Switch non momentary lt not gt Gnd Not Flaps Up i NEUEN gt 17V Inhibit J1 36 28V_DISC_04 28V Audio Inhibit Discrete 6 6 17 44 AV Not Inhibit m Gnd Inhibit J1 17 GND_DISC_04 GND Audio Inhibit Discrete 6 6 16 lt not gt Gnd Not Inhibit J1 35 28V DISC 05 28V Landing Gear Discrete 6 6 3 2 4 6 2 6 7 s ICE o eue o nec s ee GPWS Warning Discrete 741 41 78 DISC_OUT_1 Output Terrain Awareness Warning 147 2 Obstacle Awareness Warning PRU GPWS Alert Discrete 741 41 77 DISC_OUT_2 Output Terrain Awareness Caution 747 1 Obstacle Awareness Caution IU DISC OUT 3 Glideslope Cancel Discrete 28V DISC 11 J1 46 GND_DISC_05 GND Landing Gear Discrete p J1 15 GND_DISC_06 Glideslope Cancel Discrete Note 1 6 6 13 22 2 i GND DISC 07 Input NotDefinedinthisID Note3 28V DISC 13 Input NotDefinedinthis ID Note 3 Configuration Data Lamp Format Flashing Lamps Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 268 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 14 Category 14 Audio Output Level The following table provides identification of the Audio O
317. lation kits can interfere with the GPS antenna connector for this reason a new J1 backshell is supplied with MK VI VIII installation kits 3 2 4 Analog and Digital Inputs The analog and digital inputs to the MK VI VIII EGPWS are defined as the Categories are selected Instructions for documenting these interfaces are provided with the Category selection instructions 3 2 5 Discrete Inputs The discrete inputs are defined in Appendix E Section 6 6 Additional information for some discretes is provided within the Category in which they are used 3 2 6 Serial Outputs The EGPWC provides for ARINC 453 and ARINC 429 serial outputs Terrain display data is output on two ARINC 453 channels when the Terrain Awareness display function is enabled Low speed ARINC 429 output buses are provided by the EGPWC are described in Appendix E Section 7 ARINC 429 output data includes 1 Internal data data output for test purposes only such as internal logic booleans Geometric Altitude and Terrain Clearance information 2 Alert Warning status Voice and Lamp activity can be provided to display systems and flight recorders 3 Internal mode status 4 Terrain display messages for TAD cockpit integration Note During EGPWS Self Test the SSM of each output label is set to the Functional Test status code Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 52 Honeywell MK VI MK VII
318. lect 1 Discrete Terrain Awareness Caution or Warning _ 1 51 DISC_OUT_8 Output Obstacle Awareness Caution or Warning 7 4 7 3 Gnd Terrain Pop Up J1 49 DISC_OUT_9 Output Terrain Display Select 2 Discrete I 1 J2 15 28V_DISC_13 Not Defined in this ID Note 3 J1 50 MON_OUT_3 Output Not Defined in this ID Note 3 J1 52 DISC OUT 7 Output Not Defined in this ID Note 3 ass Flashing Lamps GPWS Warning Discrete 741 Yes J1 78 DISC_OUT_1 Output Terrain Awareness Warning 147 2 Yes Obstacle Awareness Warning Yes GPWS Alert Discrete 741 Yes J1 77 DISC_OUT_2 Output Terrain Awareness Caution M Yes 7 4 7 1 Obstacle Awareness Caution Yes Configuration Data Possible States State Type 1 2 Type 2 Flashing Lamps Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Note 4 Function is provided as an OR operation of the physical discrete and the 429 discrete word bit if configured by the display type 28V DISC 11 Input Not Defined in this ID Note 3 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 264 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 6 Input Output Discrete Type 6 CHANNEL CONN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration R
319. lidity Barometric Alt Valid 28V Outside Air Temp Format DC Total Air Temperature 23 Input Type Basic Fault Designation STATIC AIR TEMPERATURE FAULT Probe element Excitation 5 25 2 J1 25 AA 5 V Ref Temp Input J1 63 4 42 K Ohms probe element 1 44 63 Temp In 44 53 Chassis Gnd Ground GND J1 53 OAT PROBE ELEMENT Note Nominal 500 Temperature Probe only Resistance 0 C 5000 0 60 Connection example CIC Temperature Sensor P N 05257 2 wire Connect positive lead to both J1 25 and J1 63 Connect negative lead to both J1 44 and J1 53 Chassis Ground Other probes may have three contacts Airspeed No Substitute Ground Speed for Airspeed airspeed is not available with this air data aa CHANNEL PIN FUNCTION CONNECTION PIN TYPE DESIGNATION Polarity Configuration References REFERENCE Barometric Altitude io 28V_DISC_08 gt 17V Valid 6 6 22 Validity Discrete lt 4 4V Invalid 4 2 7 Configuration miss Summary Data Derive Baro Altitude Rate Analog Baro Altitude Rate is derived using Uncorrected Barometric Altitude Rate is not available with this air data source TABLE 5 3 2 5 AIR DATA INPUT SELECT 5 CHANNEL CONNECT TO ADC 1 Fault Designation AIR DATA BUS 429RX 2 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Uncorrected Baro
320. lidity Discrete 1 invalid ss Ghdeslope 1 Invalid 6 6 11 GND Glideslope Inhibit Discrete Type Switch for inhibit of Glideslope mode Signal Status Glideslope Inhibit or Not Inhibit Mode 5 will be disabled and Glideslope will not be enunciated during cockpit Self Test and the long vocabulary test if inhibited Level 6 Audio readout Inhibit gt Glideslope Inhibit True Not Inhibit gt _ Glideslope Inhibit False 6 6 12 28 V Glideslope Inhibit Discrete Type Supplied by an alternate action latching cockpit switch for inhibit of Glideslope mode Signal Status Glideslope Inhibit or Not Inhibit Mode 5 will be inhibited and Glideslope will not be enunciated during cockpit Self Test and the long vocabulary test if inhibited Level 6 Audio readout reas Inhibit gt 28 Volts Glideslope Inhibit True Discrete Not Inhibit gt 28 Volts Glideslope Inhibit False 6 6 13 Glideslope Cancel Discrete Type Supplied by a momentary actuated cockpit Glideslope mode manual inhibit switch Signal Status Glideslope is canceled if Glideslope function is active Fault monitoring Activation of this input for more than 15 seconds will result in the Glideslope Cancel Invalid fault which will cause a GPW INOP indication Typically the Glideslope cancel can only be selected below 2000 feet AGL Level 6 Audio readout Cancel gt Glideslope Canceled Cancel Diners No
321. lingford Ave North Seattle WA 98103 Ph 206 634 2540 Burbank CA 818 843 1000 Brighton MA 616 787 1555 BF Goodrich Aircraft Sensors 14300 Judicial Road Burnsville MN 55306 4898 Ph 952 892 4000 Fax 952 892 4800 1000 Shames Drive Westbury New York 11590 Ph 516 876 8400 Fax 516 876 9153 12920 Park Street Sante Fe Springs CA 90670 Ph 562 946 6694 Fax 562 946 5150 2525 Santa Anna Ave Dallas Texas 75228 Ph 800 527 2581 Lighted Switches Displays 1640 Monrovia Avenue Costa Mesa CA 92627 Ph 800 300 9320 5505 E Rutter Ave Spokane WA 99212 1333 Ph 800 235 3300 DWG NO 060 4314 150 REV http www amp com http www amphenol com http www avidyne com http www avtcorp com United Kingdom Surrey England 44 0932 22 4122 Germany Raunheim Germany 49 6142 43077 8 9 http www bfg aerospace com Email info computerinstruments com http www computerinstruments com Email sales comant com http www comant com distributor for Eaton switches http www dallasavionics com http www aerospace eaton com distributor for STACO switches http www edmo com SHEET 150 Honeywell MK VI MK VIII EGPWS Installation Design Guide Electronic Cable Specialists and Electrical Conservation Systems Inc Electrical amp Mechanical Technologies EMTEQ Hollingsead International IDD Aerospace ITT Cannon Korry Electronics Master Specialties Co Mid Co
322. ll Display pus type Picture Bus or ARINC 453 CHANNEL TX453 1 CONNECT TO 5 d Indicates the correct connection for these pins CHANNEL TX453 2 CONNECT TO i Indicates the correct connection for these pins Notes 1 Peaks Mode Not Available or Elevations via overlay shown here Peaks mode Not Available means that this display type cannot display Peaks Mode Overlay Page Table 3 8 2 1 Definition of Display Configuration Group Tables Appendix E Section 5 3 6 3 8 3 Display Input Control Group This input bus is connected to the display or display controller and transmits Range settings Display Mode and Display status to the MK VI MK VIII EGPWC In some installations where the terrain display s is controlled from one source controller the Range inputs to the EGPWS must be paralleled to satisfy dual input requirements of the EGPWS Display Input Control Group iu ST a 429 422RX 1 WXR Output 429 bus 1 Bus Type Basic 429RX 3 WXR Output 429 bus 1 Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms Range Status Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 70 Honeywell MK VI MK VIII EGPWS Installation Design Guide In some installations where the Radar Terrain displays are controlled from one source the Range input buses into the EGPWS must be paralleled to
323. ll MK VI MK VIII EGPWS Installation Design Guide first of type installations for these installations all sections of the Flight Test procedure shall be performed Precedence has been established for testing only the Terrain Awareness functions when replacing an existing MK VI GPWS Installers should contact their local FAA office for confirmation of this approach For follow on installations of the same aircraft type and interface the flight test is not required When updating an STC to the current part number it is only necessary to flight test significant new features The notice of change is available in Honeywell Service Bulletins Suggestions for recording of the EGPWS data during a Flight Test for follow on analysis In WinViews change the recording Sample Rate to 1 second intervals WinViews Terminal Mode Options Settings 1000 This sample rate will record adequate data for future analysis e Continue recording between tests Missing data is aggravating Recording in flight between test sites hundreds of miles apart is not necessary but continuous recording when Mode 1 ends and Mode 4 begins is helpful Recording of the take off from brakes locked through climb out also aids later analysis as does continuous recording of approach to aircraft off the runway e The WinViews software program records in 1 44 megabyte files that can be transferred from Laptop computer to other computers with ease Using 1 second sample rate the E
324. low UNIVERSAL TIME CORRELATION BIT ASSIGNMENTS BIT NO DEFINITION CFDS GPS DEFINITION CAIMS 11 14 Tenths of Minutes JNITS of Minutes ENS of Minutes of Hours ENS of Hours N A 6 2 18 Date 260 GPS LABEL Octal 260 Units Day Month Year Max Range N A Approx LSB 1 Day NOTE 1 BITS 11 to 14 4 UNITS of the YEAR 0 to 9 BITS 15 to 18 4 TENS of the YEAR 0 to 9 BITS 19 to 22 4 UNITS of the MONTH 0 to 9 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 280 Honeywell MK VI MK VIII EGPWS Installation Design Guide BIT 23 1 TENS of the MONTH 0 or 1 BITS 24 to 27 4 UNITS of the DAY 0 to 9 BITS 28 to 29 2 TENS of the DAY 0 to 3 6 2 19 Control Word 154 MFD Approx LSB N A Sign Bit N A DAU WORD BIT ASSIGNMENTS Bit No DEFINITION 11 13 Not Used by EGPWC 14 Terrain Display Overlay Active 15 29 Not Used by EGPWC 6 2 20 Control Word 2 271 273 CONTROL WORD 2 WXR Source WXR Control Panel Nav Display DISPLAY WD 1 DISPLAY BUS LABEL Octal 271 Units N A Max Range N A Approx LSB N A For FDS 255 display the label is 273 Data Bits Discrete word see below Sign Bit N A Pad Bits 9 10 Transmit Interval mSec 100 to 120 ms Data Type Discrete SDI Bits N A CONTROL WORD 2 BIT ASSIGNMENTS BITS 24 to 29 Display Range 5 to 320NM format as follows _
325. lso contained on an ARINC 429 output word Note Some display systems provide one message area for both warning and associated INOP annunciation There are conditions where GPW INOP and a GPWS warning can exist at the same time e g Sinkrate warning can occur even if a Ground Airspeed input fault exists For these installations a configuration item JNOP amp Warning Annunciation in Same Window is provided which causes the INOP annunciation to extinguish whenever a valid warning annunciation is required Various formats of monitor outputs can be provided as defined in Category 13 7 4 4 Terrain Display Switching Discretes WxR EGPWS Display Select The EGPWC produces two discrete outputs for controlling the terrain display s They can be used either to control picture bus switching relay s or connected directly to the symbol generator s 7 4 5 Flap Override Discrete The MK VI EGPWC Flap Override function can be selected by the pilot to desensitize the alert and warning modes The Flap Override discrete output is active Gnd whenever the Flap Override has been selected and is typically used to drive a lamp 7 4 6 Glideslope Cancel Discrete The Glideslope Cancel discrete is active whenever Glideslope Cancel has been selected and is typically used to drive a lamp in the Glideslope Cancel switch 7 4 7 Terrain Obstacle Awareness Alert Discretes Terrain Awareness provides discrete alert outputs for Terrain Obstacle Cautions and Warnings The
326. ltimeter Receiver Transmitter Self Test output This connection is no longer required but may be left intact for retrofit installations Discrete Position Status Connector Pin Audio Inhibit 28 Inhibit 28V J1 36 Not Inhibit Gnd Open Audio Inhibit Gnd Inhibit Gnd J1 17 Not Inhibit 28V Open 3 15 1 4 Landing Gear Discrete Landing Gear discrete is supplied by the Gear or Gear handle switch The active position 28V or GND indicates Gear Down and should be connected to a contact that will indicate Gear Down when the Gear are lowered prior to 500 feet Radio altitude Discrete Position Status Connector Pin Landing Gear 28 Down 28V J1 35 Not Down Gnd Open Landing Gear Gnd Down Gnd J1 16 Not Down 28V Open For Fixed Gear aircraft the Audio Menu in Category 5 should be ID 2 or 3 and one of the following Gear Discrete arrangements should be used to simulate Gear Down to the EGPWS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 104 Honeywell MK VI MK VIII EGPWS Installation Design Guide FIXED LANDING GEAR FLOAT AIRCRAFT MK VI EGPWS ALTERNATE AIR SWITCH ARRANGEMENT COMPUTER Example Shown Twin Otter Not LANDING FULL LANDING FLAP POSITION 16 18 Landing Flap Discrete Gnd LANDING FLAPS UP APPROACH FLAP POSITION 57 77 Landing Gear Discrete 2
327. mary Power Input eee ERE Bc e P S BEA CHASSIS ssp u LR RI e 3 2 E PS Antennas m rad uei aee S 3 24 Analog and Digital Inputs anan eti etn dede 3 2 9 Discrete een teet mene edet eec 3 20 Output ET REM 3 2 8 RT a Toe e i amens 312 9 Configuration Modi le s doe eei tii gelegen erede fee 3 3 CATEGORY 1 AIRCRAFT MODE TYPE nennen 3 31 Aircraft Mode Types maa edu aod putes ded tette cerdo 3 3 2 Mode T types sio Ses E oda ea eMe GE P Ure ep ed obe d cd oe us d eb 55 Mode 2 type i tede TRE te ete iR brit 3 34 Mode 3 AY Pe sco Le UR e Ibat de tanta S u AS a tege 33 9 MO de o otis ote ees te ebat ee eb e dle ee i e e DERE ERE e 3 3 6 Bank Angle Type a a tte e ti de e ema oett ttes 3 3 7 Runway Length MK VIII EGPWS onby trente 3 9 OIISTIRUCHORS 2 oet ek EL E LEM UE 3 4 CATEGORY 2 AIR DATA INPUT SELECT ei seis aree Or RR Se EHE SUO NE re e Or EE Ce ERU 3 41 Analog Gat 2 ID 03 4 TT 42 in tbt ev eee 3
328. mp Formatiu uq a s Tea nd beet ie nd e ex eere eon p ER rectos 109 3 15 2 2 Flashing Lamps y ua anay e tee t dde E ede edet do eed dre Die 109 3 152 3 GPWS INO P Discrete erri eh Or e re M AA Re Ae 109 3 15 2 4 TAD INOP Discrete 3 15 2 5 GPWS Warnirig Discretes HERE E E b RECO Cop S Ge EE Re E dO 109 3 15 2 6 GPWS Alert Discrete 27 0 b ot pt ced d ence ttem d d tace 110 3 15 27 Glideslope Cancel d Discrete eei eere etaed inte tine de etna aysaspa ance de Tao dore ena Tn ie aun deae de eaa a ia ine S 110 3 15 28 Flap Override Dis Cr Cte acs eorom ert eer entre the dae ep Eo eR SEES RETE ER ee 3 15 29 Steep Approach Diserete Ho PERRO ean Du Ee ERE eer TRE 3 15 2 10 Audio On Discrete TCAS TAS Inhibit Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 8 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 15 2 11 Terrain Display Select 1 amp 2 Discrete enne enne enne nnet tenentes nnne 111 3 155212 Terrain Pop up Discrete eode er AEGRO ERU au Si cue 112 3 13 SANS MUCHOS eremi eee 113 3 16 CATEGORY l4 AUDO OUTPUT LEVEL
329. must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 229 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 247 Collins FDS 255 2000 with selection controlled by the EGP WS MK VIII Only Display Configuration Group 252 Display Type 7 Collins FDS 25520000 1 1 1 1 Sweep Type __ Peaks Mode Category 7 Options Select Group 1 5 3 7 Manual select Anytime Manual deselect O O Auto Range ee Moving Marker No Overlay Page Yes for Peaks Elevations only located on lower left of the display YV yu O Auto Pop Up Category 7 Options Select Group 1 Display bus type ARINC 453 DISPLAY BUS 1 CONNECT TO 453 1 58 Terrain Display data to switching relay Symbol Generator 1 2 13 J1 59 DISPLAY BUS 2 CONNECT TO 453TX 2 56 Terrain Display data to switching relay Symbol Generator 2 4 2 13 2 1 57 72 Display Input Control Group 253 CHANNEL CONNECT TO WX IND 429 Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 36 Range 6 2 20 273 N A 5 320NM Basic N A 100 CHANNEL CONNECT TO WX IND
330. n 500 ohm Temp Input Temperature Probe Chassis Ground Analog ADC vsd Cat 2 Uncorrected Baro Altitude Vendor Model ID Altitude Out Common BIT Out CIC 04077 0 J1 F J1 G J1 E Collins ADS 65 3 J1 12 J1 13 J1 5 CIC 02702 4 J1 A J1 B J1 E Honeywell AZ 241 1142 J1A 63 J1A 11 CGND J1A 12 Honeywell AZ 242 11 12 18 17 J1A 11 CGND J1A 12 Honeywell AZ 648 1142 J1 J J1 G J1 U Honeywell AZ 800 11 12 J1A 78 J1A 10 CGND J1A 34 Honeywell AZ 810 1142 J1A 78 J1A 10 CGND J1A 34 Honeywell AZ 252 11 12 J1A 17 J1A 10 CGND J1A 34 NOTES 1 The connector pin numbers given in the Table above are to the best knowledge of Honeywell EGPWS engineering Please contact the manufacturer s customer service to confirm your installation 2 ID 12 does not require an OAT input instead a constant temperature of 25 deg C is assumed 3 Honeywell AZ 810 should only be used as an analog source if it does not have a digital interface 4 Honeywell AZ 242 with part numbers 4013242 708 709 710 712 713 and 742 have DC Altitude out at pin J1B 17 Part numbers 4013242 709 and 711 have DC Altitude out at pin J1A 40 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 58 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 4 2 Digital ARINC 429 Cat 2 ID 5 1 6 13 Air Data Type 1 is a low speed digital ARINC 429 s
331. n Display data to switching relay Symbol Generator 4 2 13 2 B J1 57 72 Display Input Control Group 2 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM Basic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM Basic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CONN PIN REFERENCENAME PINFUNCTION Polarity Confipuratim J1 32 GND DISC 12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x J2 42 Integration Notes 1 When interfacing to a single di
332. n Unit DC Digital Command DDM Difference in Depth of Modulation DEVN Deviation DH Decision Height DITS Digital Information Transfer System DME Distance Measuring Equipment DO Discrete Output DSP Digital Signal Processor DSU Display Switching Unit DSWC Digital Stall Warning Computer EEPROM Electrically Erasable Programmable Read Only Memory EFCP EFIS Control Panel EFIS Electronic Flight Instrument System EGPWC Enhanced Ground Proximity Warning Computer EGPWD Enhanced Ground Proximity Warning Display EGPWS Enhanced Ground Proximity Warning System EICAS Engine Indication and Crew Alert System EMI Electromagnetic Interference ENB Enabled EPROM Erasable Programmable Read Only Memory F T Functional test F W Fail Warning Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 324 Honeywell MK VI MK VIII EGPWS Installation Design Guide Acronym Interpretation FAA Federal Aviation Administration FCC Flight Control Computer FDR Flight Data Recorder FIAS Flight Inspection Aircraft System FMC Flight Management Computer FMS Flight Management System FPM Feet per Minute FSEU Flaps Slats Electronic Unit FWC Fault Warning Computer G S Glideslope GMT Greenwich Mean Time GPS Global Position System GPW Ground Proximity Warning GPWS Ground Proximity Warning System GT Greater Than H W Hardware HDG Heading HDOP Horizontal Dilution of Position HFOM Horizontal F
333. n the PC serial port connector with standard DB9 and the EGPWC 5 232 interface is defined as follows RS232 Receive RS232 RS 232 Ground NOTE Some PC Comm Ports have Pins 2 amp 3 reversed from what is described above Connector AMP 204513 2 Pin Contact 204370 2 QTY 4 Connector AMP 205161 1 M39029 58 360 Socket Contact AMP 205090 1 QTY 3 Backshell AMP 745854 5 M39029 63 368 Jackscrew AMP 747784 3 Grommet Set AMP 747746 1 P3 EE a a a i Length as required 5 to 50 Alternate part number 748364 1 connector and 748333 4 or 7 pin contact Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 118 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 4 3 WinVIEWS Windows Virtual Interface to the Enhanced Warning System WinVIEWS is a software tool developed by Honeywell to communicate with the EGPWS WinVIEWS provides a detailed status of the software configuration and input signals which enables quick identification of system configuration and is utilized for programming the system Configuration Module To obtain a copy of the WinVIEWS software contact Honeywell of Honeywell Aerospace Electronic Systems Aerospace Electronic Systems PO Box 97001 PO Box 97001 Redmond WA 98073 9701 USA Redmond WA 98073 9701 USA Attn Order Administration M S 33 Attn EGPWS Applications Engi
334. n the harness to allow water droplets that might form on the harness due to condensation to drip off at the bend and not collect in the connector NOTE For retrofit installations of classic MK VI GPWS and installing a EGPWS with internal GPS the connector backshell of the classic MK VI P1 connector will interfere with the GPS antenna connector on the front of the EGPWS The connector backshells chosen for the EGPWS kits now extends straight out and does not interfere with the GPS antenna connector The length of cables from the EGPWS connectors to other system units is not generally critical because unit interfaces are designed with high impedance inputs low impedance outputs and low noise susceptibility characteristics The exception is the wires from the EGPWS Configuration Module which was designed to be a part of the EGPWS connector backshell because of the requirement for short lead length Follow aircraft manufacturer s sub system manufacturer s or ARINC specifications for shield grounding 2 3 3 MK VI VIII Computer Installation The MK VI and MK VIII EGPWS installation will conform to standards designated by the customer installing agency and existing conditions as to the unit location and type of installation However the following suggestions will assure a more satisfactory performance from the equipment A Plana location on the aircraft so that EGPWS is accessible for front panel maintenance controls Check to be sure
335. n title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 256 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 12 Category 12 Windshear Input Select The following table provides identification of the Windshear Input Type The entry in the Windshear Input Type corresponds to a table that provides detailed information on the configuration For example the details for Windshear Input Type 255 are found in 5 3 12 255 In this category only the following signals are to be defined Body Angle of Attack AOA in ARINC 429 format e Normalized Angle of Attack AOA in ARINC 429 format Table 5 3 12 Windshear Input Select Windshear Description Windshear Windshear Windshear Windshear Software EGPWS Input Type Disable INOP Caution Caution Voice Effectivity Effectivity Disable Disable Disable MKVI N A No Windshear TRUE TRUE TRUE TRUE 020 X Digital ARINC 429 255 AOA via Dual FALSE FALSE TRUE TRUE 020 buses Note 1 Digital ARINC 429 AOA via Dual IOC FALSE FALSE buses Note 1 Digital ARINC 429 AOA via Dual IOC FALSE FALSE buses Note 1 Note 1 IDs 253 254 and 255 may only be used in conjunction with other IOC bus selections for categories 2 6 8 9 10 and 11 Table 5 3 12 255 Windshear Input Type 255 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429RX 1 Format ARINC 429 Hig
336. nal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM Basic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Mode Display Word 1 6 2 26 Discrete Mode Tilt Gain Basic N A Range Display Word 2 6 2 20 Discrete 5 320NM Basic N A Discrete Word Vertical Profile 6 2 27 Discrete VP Mode Bit 11 Basic N A CONN PIN REFERENCENAME PINFUNCTION Polariy Confipuratim J1 32 GND DISC 12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x 2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 0
337. nal Type Resolution Rate ms A J2 23 Magnetic Heading 6 2 32 320 15 180 degrees Basic 0 0054931640625 10 20 2 6 True Heading 6 2 37 314 15 180 degrees Basic 0 005493 1640625 25 50 Table 5 3 11 254 Heading Input Select 254 CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 422RX_1 Format ARINC 429 High Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 37 True Heading 6 2 32 314 15 180 degrees Basic 0 005493 1640625 25 50 B J2 36 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Tvpe Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 41 True Heading 6 2 32 314 15 180 degrees Basic 0 005493 1640625 25 50 12 40 Table 5 3 11 255 Heading Input Select 255 CHANNEL CONNECT TO IOC 1 Fault Designation IOC BUS 1 429 422RX_1 Format ARINC 429 High Speed Bus Type Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 37 Magnetic Heading 6 2 32 320 15 180 degrees Basic 0 005493 1640625 25 50 12 36 pe Basic Data Reference Label Sig Bits Range Signal Type Resolution Rate ms A J2 41 Magnetic Heading 6 2 32 320 15 180 degrees Basic 0 005493 1640625 25 50 J2 40 CHANNEL CONNECT TO IOC 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus T Proprietary notice o
338. nalog Barometric Aitae _ Airspeed input DCAmdog lt Analog ArTemperaue dd Abg lt Localizar Validity Discrete 28000 Test Point 3 Test point 11 49 Lampout gt gnd va Select palav Output on Test Point 4 Test point J1 50 Monitor Out gt gnd Windshear Inop Lamp Output monitor Test Point 5 Test point 1 51 Lampout gt Terrain Pop Up Discrete Output Test Point 6 Test point J1 52 Lampout gt gnd Test Point 7 Test point Sz J1 53 Temperature Probe GND Test Point 8 Test point EN J1 54 Lampout gnd T Select Relay Output Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 132 Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name GPWS 965 0686 001 020 Signal Type lt uon 5 Signal VIII EGPWS Enhanced Test Ponta 4510u 5 Teman Display Output Data 1 Bleo Power Input GND PwReno X PWRL Power Input 26vDC retur Barometric Altitude Rate ipu DC Amaogt lt Analog Barometric C Airspeed Inot 9 Air Temperature E CIE _ Reewd
339. ncel Discrete 746 ss J1 73 DISC OUT 4 Output Windshear Warning Discrete 7410 J1 52 DISC OUT 7 Output Windshear Caution Discrete TAM fo J1 69 DISC OUT 5 Output Audio On Discrete i742 DISC_OUT_6 Terrain Display Select 1 Discrete Terrain Awareness Caution or Warning J1 51 DISC OUT 8 Output Obstacle Awareness Caution or Warina 7 4 7 3 Gnd Terrain Pop Up DISC_OUT_9 Terrain Display Select 2 Discrete 4148 28V DISC ii put 4114 GND DISC O7 Input NotDefmedintisID Note3 245 28V DISC i3 put Not Defined in this 1D Note 3 Note 1 Provided by Momentary cockpit switch non latching Note 2 Provided by Alternate cockpit switch Latching with guard if inhibiting Note 3 This discrete may be used in another category Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 267 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 255 Input Output Discrete Type 255 CHANNEL CONN PIN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE ROSE gt 17V Inhibit J1 38 28V_DISC_02 28V Glideslope Inhibit Discrete 6 6 12 44 AV Not Inhibit mom Gnd Inhibit J1 19 GND_DISC_02 GND Glideslope Inhibit Discrete 6 6 11 lt not gt Gnd Not Inhibit 28V Landing Flaps Discrete gt 17V Flaps Up uad 28 See Flap Override Switch non momentary lt 4 4V Not Flaps Up E GND Landing F
340. nded for remote switching through the aircraft and are therefore subject to being connected to other signals and are also subject to transient voltage conditions For these reasons the following rules apply to each input unless otherwise stated Each input is capable of withstanding voltage transients of 600VDC for 10 us and 50VDC continuously without damage The 28 VDC discretes are internally biased via a pull down resistor and are externally pulled up to 28VDC when active The characteristics of each 28 VDC discrete input are as follows 28 VDC Discrete Characteristics Quantity 13 Active Voltage Range Logic True gt 17 VDC Inactive Voltage Range Logic False lt 4 4 VDC Diode Isolation None Input Impedance gt 95 Maximum Fault Current lt 60 uA Pin Assignment Signal Mnemonic See specific discrete in Category 13 28V_DISC The Ground discretes are internally biased via a pull up resistor and are externally pulled down to ground when active The characteristics of each Ground discrete input are as follows Ground Discrete Characteristics Quantity 15 Active Voltage Range Logic True lt 3 VDC Inactive Voltage Range Logic False gt 100 KQ to ground or gt 3 5 VDC Diode Isolation Each input is diode isolated to prevent current sinking Input Impedance gt 10KQ Maximum Fault Current lt 100 uA at 28 VDC input Pin Assignment Signal Mnemonic See specific discrete in Category 13 GND_DIS
341. neering Phone 425 885 8719 Phone 425 885 3711 FAX 425 885 8988 425 885 2994 GPWS Hotline 800 813 2099 WinVIEWS be sent via e mail when e mail address is provided 4 4 4 WinVIEWS Operation Connect the PC to the EGPWC using the RS 232 cable as described in section 4 4 2 On the PC start Windows 3 1 or higher Start the WinVIEWS EXE program Use F6 to select the Terminal Mode Various commands are available in this mode Type HELP or for a list of the commands available mU EM 4 5 Configuration Module Programming The EGPWC reads the aircraft configuration from the Configuration Module which is installed in the EGPWC connector The Configuration Module must have the aircraft specific configuration ID string written to it before the EGPWS is operational The ID string is defined by 15 separate categories listed in Appendix E Table 5 2 Category ID Selection Procedure For programming the Configuration Module the following procedure is used 1 Verify EGPWC interface to P2 connector including Configuration Module and RS 232 interface PC 2 Power EGPWC and PC and start WinVIEWS 3 With WinVIEWS active in the Terminal Mode configuration sub mode commands are available for programming purpose Type CFG at the Terminal Mode prompt gt At this point the CFG prompt is displayed and the program and EGPWC are ready for entering the program command and data string Type
342. nfiguration A definition of each of the entries in the Display Configuration Group tables is provided in the table below Display Type Display manufacturer model etc Sweep Type The type of sweep used for terrain data fan standard etc Auto Pop Up Category 7 Options Select Group 1 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True The TA amp D Alternate Pop Up is set to The TA amp D Alternate Pop Up is set to False or True in Category 7 If False False or True in Category 7 If True Pop Up behavior for the terrain Pop Up behavior for the terrain display is described here display is described here Peaks Mode Category 7 Options Select Group 1 See Note 1 Peaks Enable False Peaks Enable True Peaks Enable is set to False or True Peaks Enable is set to False or True in Category 7 The effect of setting it in Category 7 The effect of setting it to False is described here to True is described here Manual select Describes if when terrain display s can be manually selected Manual deselect Describes if when terrain display s can be manually deselected Auto Range Defines if the display data is automatically scaled and if so the scale used such as 10 nautical miles Moving Marker Indicates whether or not a moving marker is provided Describes where TERR and Peaks Elevations overlays will be located on the display screen Defines the display bus type KC Picture Bus KCPB was ASPB Honeywe
343. nformation beyond Internal and External Current Faults in order to help isolate the reason for certain EGP WC INOP situations These messages will be read out during Present Status on the RS 232 interface or voice output during Self Test Level 2 The table below defines the System Status Messages TABLE 7 5 1 1 EGPWC SYSTEM STATUS MESSAGES System Level Event INTERNAL INDICATIONS System Status Message TRUE 3INOP TRUE TAD Deselected Terrain Awareness INOP 2 TAINOP TRUE Terrain Awareness INOP Terrain Clearance Floor TCFINOP TRUE Terrain Clearance Floor INOP INOP 3 Always Created Position Error AND TCFINOP TRUE Terrain Clearance Floor Position Error Terrain Not Available 4 TAD Position Error AND TAINOP FALSE Terrain Awareness Position Error Outside Regional Database TRUE MK VI Terrain Awareness Outside Regional Terrain ONLY Database Windshear INOP 5 WSINOP TRUE Windshear INOP lt The following preconditions apply a The signal must not be faulted since if faulted signal fault message will exist b TAD TCF Inhibit Discrete is NOT selected c TAD Disable program pin is NOT selected d The signal condition must NOT be masked via the configuration database and both On Ground and In Air masks must be taken into account e The associated input signal must exist for the current aircraft configuration 2 TAD INOP Preconditions a TAD TCF Inhibit Discrete NOT selected and b TAD
344. ng and Inspecting the Equipment Exercise extreme caution when unpacking equipment Perform a visual inspection of the unit for evidence of damage incurred during shipment If a damage claim must be filed save the shipping container and all packing materials to substantiate your claim The claim should be filed as soon as possible The shipping container and all packing materials should be retained in the event that storage or reshipment of the equipment is necessary 2 3 Equipment Installation 2 3 1 General The following paragraphs contain information pertaining to the installation of the MK VI and MK VIII EGPWS including instructions concerning the location and mounting of the equipment The equipment should be installed in the aircraft in a manner consistent with acceptable workmanship and engineering practices and in accordance with the instructions set forth in this publication To ensure the system has been properly and safely installed in the aircraft the installer should make a thorough visual inspection and conduct an overall operational check of the system on the ground prior to flight CAUTION AFTER INSTALLATION OF THE CABLING AND BEFORE INSTALLATION OF THE EQUIPMENT A CHECK SHOULD BE MADE WITH THE AIRCRAFT PRIMARY POWER SUPPLIED TO THE MOUNTING CONNECTOR TO ENSURE THAT POWER IS APPLIED ONLY TO THE PINS SPECIFIED IN THE INTERWIRING DIAGRAMS IN SECTION III 2 3 2 MK VI MK VIII Computer Location Care should be exercised to avo
345. nhibit enable or disable Fault Monitoring Activation of this input will result in the External EGPWS Inhibited Level 6 Audio readout n Inhibit gt 28 Volts Audio Inhibit sey Not Inhibit gt 28 Volts Audio Not Inhibit 6 6 18 Display Select Discrete 1 Type Supplied by momentarily actuated cockpit manual switch Signal Status Terrain Awareness Display TAD activated if not active TAD canceled if currently active Level 6 Audio readout True gt Display Discrete 1 True Display Select Discrete 1 False gt Display Discrete 1 False Proprietary notice on title page applies CAGE CODE 97896 SCALE SIZE A DWG NO 060 4314 150 SHEET 300 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 6 19 Display Select Discrete 2 Type Supplied by momentarily actuated cockpit manual switch Signal Status Terrain Awareness Display TAD activated if not active TAD canceled if currently active Level 6 Audio readout True gt Display Discrete 2 True Display Select Discrete 2 False gt Display Discrete 2 False 6 6 20 Terrain Awareness amp TCF Inhibit Discrete Type Supplied by an alternate action latching and self indicating cockpit switch for inhibit of Terrain Awareness amp TCF functions Signal Status Terrain Awareness amp TCF Inhibit or Not Inhibit Terrain Inhibited will be enunciated during cock
346. ntinent Instruments Norwich Aero Products PIC Wire amp Cable Supply Positronic Industries Sensor Systems Inc Shadin Co Spirent Systems Penny amp Giles Aerospace Staco Switch see EDMO Distributors CAGE CODE 97896 SCALE NONE SIZE A 5300 W Franklin Drive Franklin WI 53132 8642 414 421 5300 584 W18693 Enterprise Drive Muskego WI 53150 PH 262 679 6170 Fax 262 679 6175 888 679 6170 Sante Fe Springs CA 213 921 3436 Redmond WA 425 885 4353 Santa Ana CA 714 557 4700 901 Dexter Avenue North Seattle WA Ph 800 257 8921 Fax 206 281 3576 Costa Mesa CA 714 642 2427 N53 W24747 S Corporate Circle P O Box 330 Sussex WI 53089 0330 414 246 0500 Fax 414 246 0450 423 North Campbell Avenue Springfield Missouri 65801 8929 Fullbright Avenue Chatsworth CA 91311 818 341 5366 Fax 818 341 9059 6831 Oxford Street St Louis Park MN 55426 Ph 800 328 0584 Fax 612 924 1111 8710 E 32 Street N Wichita KS 67226 Ph 316 636 2000 Fax 316 636 9098 1139 Baker Street Costa Mesa CA 92626 4191 Ph 714 549 3041 Fax 714 549 0930 DWG NO 060 4314 150 REV http www ecsdirect com Email Sales emteq com http www emteq com http www hollingsead com Email info korry com http www korry com http midcontinentinstruments com http www norwichaero com Email BHackett Picwire com http www picwire com Email info positronic com http www posi
347. ny Mode 1 Sinkrate Mode 3 Don t Sink Mode 4 Too Low Gear Too Low Flaps Too Low Terrain Mode 5 Glideslope Terrain Awareness caution or Obstacle Awareness caution This feature activates a GPWS amber lamp located in the cockpit within sight of each pilot 3 15 2 7 Glideslope Cancel d Discrete Optional Glideslope Cancel d discrete J1 76 will activate when the Glideslope Cancel discrete momentary has been pressed any time below 2000 feet Radio Altitude if the ILS is tuned This feature activates a G S CANCLD amber lamp located in the cockpit within sight of the pilots 3 15 2 8 Flap Override Discrete Optional Flap Override discrete J1 73 will activate after either pilot has initiated the manual selection of the Flap Override momentary discrete This feature activates GPWS FLAP OVRD blue lamp located in the cockpit within sight of the pilots The lamp serves to remind the flight crew that this function is active 3 15 2 9 Steep Approach Discrete Steep Approach discrete J1 52 will activate when the Steep Approach discrete momentary action has been pressed This feature activates a STP APR amber lamp located within sight of the pilots 3 15 2 10 Audio On Discrete TCAS TAS Inhibit Optional Audio On discrete J1 69 will activate during any EGPWS voice annunciation This output is used to inhibit other systems such as TCAS or TAS from talking during EGPWS annunciation This feature does not have a lamp asso
348. ode 4A Gear Down Mode 4B Flaps Down Mode 4 A B A B Alternate Mode 4B at 500 ft lt X knots feet lt X knots Maximum Type GA Fast Normal Mode 4B 178 knots 170 ft 150 knots 750 ft 6 GA Fast Alternate Mode 4B 178 knots 150 ft 148 knots 750 ft 8 GA Slow Normal Mode 4B 148 knots 170 ft 120 knots 750 ft 7 GA Slow Alternate Mode 4B 148 knots 150 ft 118 knots 750 ft 9 GA Fast MK II emulation 178 knots 200 ft 148 knots 1000 ft 5 Bizjet MK V VII emulation 190 knots 245 ft 159 knots 1000 ft 1 NOTE 1 Some installations that have chosen the GA SLOW aircraft type have found during flight test that the aircraft can not or does not slow to less than 120 knots on normal approach Thus the installation is prone to nuisance TOO LOW TERRAIN alerts These installations should choose the GA FAST aircraft type 3 3 6 Bank Angle Type Two Bank Angle callout curves are defined GA Turboprop and Bizjet Turbofan Both Bank Angle callout curves have an Autopilot Engaged warning area The Bizjet Turbofan Bank Angle callout curve is equivalent to the MK V and MK VII EGPWS Bank Angle callout curves when the autopilot is not engaged Aircraft Type Lower Cutoff Lower Boundary Upper Boundary Slope GA Turboprop 10 ft 10 ft 15 210 ft 50 2450 ft 50 Bizjet Turbofan 5 ft 30 ft 10 150 ft 40 2450 ft 55 Proprietary notice on title page applies SCALE NONE SIZE A CAGE CO
349. olution Rate ms J2 28 cm Latitude 6 4 1 32 180 Degrees Basic single precision 1000 J2 29 Rx Longitude 6 4 1 32 180 Degrees Basic single precision 1000 HP Error 6 4 1 meters Basic single precision 1000 Altitude 6 4 2 meters Basic single precision 1000 VP Error 6 4 2 meters Basic single precision 1000 Ground Speed 6 4 3 meters sec Basic single precision 1000 True Track Angle 6 4 3 360 Degrees Basic single precision 1000 East Velocity 6 4 4 meters sec Basic single precision 1000 North Velocity 6 4 4 meters sec Basic single precision 1000 Vertical Velocity 6 4 4 meters sec Basic single precision 1000 GPS State 6 4 5 Discrete Wd Basic n a 1000 Integrity State 6 4 5 Discrete Wd Basic n a 1000 Error Status 6 4 5 Discrete Wd Basic n a 1000 Notes Slowest acceptable update rate in milliseconds Table 5 3 3 4 Position Input Type 4 High Speed ARINC 743A GPS CHANNEL CONNECT TO GPS ARINC 743A Fault Designation GPS BUS 429RX 4 Format ARINC 429 High Speed Bus Type Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 5180 Degrees Basic 0 00017166137695 1000 Longitude Normal 6 2 8 5180 Degrees Basic 0 00017166137695 1000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 1000 Altitude 6 2 4 E131 072 FT Basic 0 125 1000 VFOM 6 2 13 32768 ft Basic 0 125 1000 HFOM 6 2 10 16 nm Basic 0 000061035 1000 Ground Speed 6 2 6 4096 Knots Basic 0 125 1000 True Track Angle 6
350. on mode and a turn is not in progress 4 approach RAIM unavailable Set when RAIM is unavailable in approach mode This flag allows a host to do a crosscheck on the RAIM prediction result before it switches into approach mode However if the system is not currently using altitude aiding this flag could be unnecessarily set and contradict with the RAIM prediction result which may assume altitude aiding Consequently the host should disregard this flag when the predicted approach RAIM is available the current NAV mode is not approach altitude aiding is not in effect and all satellites in the XPRESS visibility list are in a tracking state 5 FDE unavailable Set when FDE is not available in the current navigation mode If the FDE becomes unavailable because of shading during a turn it will be masked for the duration of the turn 6 FE active Set when FDE excludes a tracking satellite 7 Pseudo integrity warning Set when a RAIM error is detected whether or not RAIM is available in the current navigation mode Masked Integrity Warning True when there is a RAIM detected error or when RAIM is not available and a turn is not in progress Bad Coverage True when there is insufficient satellite coverage for RAIM or NAV Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 294 Honeywell MK VI MK VIII EGPWS Installation Design Guide NAV Mode binary 0 en route 1 te
351. on number of the Application software 1 2 Purpose The Interface Description Document describes all of the system external interfaces for the MK VI and MK VIII Enhanced Ground Proximity Warning System EGPWS 1 3 System Overview Refer to the EGPWS Product Specification document referenced in section 2 1 4 Document Overview This document is organized as follows Section 2 Referenced Documents 2 REFERENCES MK VI MK VIII EGPWS Product Specification 965 1180 601 MK VI MK VIII EGPWS Pilot Guide 060 4314 000 MK VI MK VIII EGPWS Line Maintenance Manual 060 4199 180 MK VI MK VIII EGPWS Terrain Database 060 4326 000 EGPWS Interface Methodology 060 4303 000 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 159 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 MECHANICAL INTERFACE 3 4 Weight The maximum weight for all MK VI and MK VIII EGPWC part numbers is 3 9 pounds 3 2 System Interface Components Refer to section 3 3 for outline drawings 3 2 1 EGPWC Mounting The mounting rack for the EGPWC is identified as follows Honeywell P N Source Vendor Vendor Part Number 405 0383 001 Bendix King 071 04003 0002 3 2 2 EGPWC Connectors There are two connectors that interface the aircraft with the MK VI and MK VIII EGPWC The 78 pin J1 and 50 pin 72 front panel interface connectors of the MK VI and VIII EGPWC contain all the interfaces for signals and
352. on title page applies CAGE CODE SHEET 81 060 4314 150 REV DWG NO A NONE SIZE SCALE 97896 Honeywell MK VI MK VIII EGPWS Installation Design Guide L LZ LOZ IXM SulllOO PSA LOZ IXM sng duie1 AgZ 159 sng HMd SMd93 A82 O YOZ L HO UO SL y sng Ionuoo LOZ IXM Sumo XYM JO 020 0X2 1 896 IIIA MIN J9 10 020 0 1 996 IA dONI uqiuu ano Aejdsig osjes ejdsiq g V INO Z O9PIA ONISV 8 V INO L O9PIA ONIHV 8 V ul zit ONINV g V ul ONIHV SMd94 Proprietary notice on title page applies CAGE CODE 97896 DWG NO 060 4314 150 REV SHEET 82 SCALE NONE SIZE A JO 020 0X2 1 896 068 078 66 2 116 JO 020 0 11 996 MIN ur O1d Sul OO ees s ejdSIp SUI OD Jo pue 103 Honeywell MKVI MK VIII EGPWS Installation Design Guide pSsA dsu lloO g V eJnj9ld ONISV NO g ONINV V 0S8 078 dXM Iud XM 51109 g ONINV V NO g V 0S8 078 dXM XM 541109 eJnj9ld ONISV sng A8C sng
353. only Mode 5 Glideslope message will activate the alert lamp output amber All other messages will activate the warning lamp output red Note that Mode 6 does not activate any lamp outputs only voices With Lamp Format 2 only the messages containing the phrase Pull Up will activate the warning lamp output red All other messages will activate the alert lamp output amber The Glideslope Cancel Input Discrete controls the output of the Mode 5 Glideslope message If the Glideslope Cancel Input Discrete is activated then the caution lamp amber and the voice annunciation will be inhibited for the Mode 5 Glideslope message Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 315 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 4 2 Audio On Discrete The Audio On discrete goes true whenever any voice message is being enunciated It will stay true until the voice is completed This output can be used to inhibit other audio systems e g TCAS during EGPWS audio or used to drive the audio key line input provided on some aircraft audio systems 7 4 3 Monitor Discretes GPWS amp Terrain or Terrain Not Available The EGPWC produces two discrete monitor outputs These discretes reflect the GPWS INOP and Terrain INOP Terrain Not Available functions These discretes activate with loss of EGPWC power The status of these two discretes is a
354. only the following signals are defined e Radio Altitude source selection input scaling and associated validities Table 5 3 8 Radio Altitude Input Select Radio Altitude Deseripuon Software EGPWS Type P Effectivity Effectivity Table 5 3 8 x MKVI MKVIII Analog Radio Altitude ARINC 552 0 0 2 2 Digital Radio Altitude ARINC 429 00 _ 3 3 Analog Radio Altitude RT 200 300 020 4 4 ____ Analog Radio Altitude KRA 405 00 Digital Radio Altitude ARINC 429 via dual IOC buses with DH MDA Note 1 3 j SEN buses Note 1 3 ef e rere e om buses with DH discrete Note 1 Digital Radio Altitude and MDA ARINC 429 EINEN CRECEN EINEN e j buses Note 1 3 Note 1 ID 251 255 may only be used in conjunction with other IOC bus selections for categories 2 6 9 10 11 and 12 Note 2 ID 254 must be used in conjunction with Category 9 ID 254 since this provides Label 163 which determines from bits 19 21 whether MDA or DH is displayed Note 3 ID 251 252 254 and 255 must not be used in conjunction with Category 4 ID 100 or 101 Altitude Callouts types Table 5 3 8 0 Radio Altitude Input Select Type 0 ARINC 552 SUMMARY DATA Format ARINC 552 with Validity Flag Radio Altimeter 1 11 64 A Input Type Basic J1 45 2 3 Fault Designation RADIO ALTIMETER FAULT Validity Radio Altitude Valid Discrete 1 28V REFERENCE
355. ons Section 5 2 describes how the Category ID s are selected and programmed for the interface to aircraft sensors and EGPWS functional options Section 5 3 and its sub sections define the specific aircraft interfaces available for the MK VI and MK VIII EGPWS 5 1 Configuration Types The selection of the basic interfaces to the MK VI and MK VIII EGPWS can be found in the following categories Aircraft Mode Type Select Category 1 Air Data Input Select Category 2 Position Input Select Category 3 Altitude Callouts Category 4 Audio Menu Select Category 5 Terrain Display Select Category 6 Options Select Group 1 Category 7 Radio Altitude Input Select Category 8 Navigation Input Select Category 9 Attitude Input Select Category 10 Heading Input Select Category 11 Windshear Input Select Category 12 I O Discretes Select Category 13 Audio Output Level Category 14 Future Configuration Category Category 15 Future Configuration Category Category 16 Future Configuration Category Category 17 5 2 Configuration Selection Each category provides information relative to aircraft interfaces or EGP WS functional options required or used for EGPWS operation Each category must be defined for the specific aircraft application according to the available aircraft sensors or equipment and the intended EGPWS function The choices provided are available in each category identified by an ID number The ID number is selected for each category and is used to load th
356. ontrol to decrease the Mode 6 Volume level under normal conditions and automatically increase Mode 6 volume 6dB when the cabin noise increases due to the windshield wipers being on Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 106 3 15 1 8 Autopilot Engaged Discrete Honeywell MK VI MK VIII EGPWS Installation Design Guide Discrete Position Status Connector Pin Mode 6 Low Volume Low Volume Gnd Not Low Volume Open J1 13 For airplanes fitted with an Autopilot additional Bank Angle mode protection is provided when the Autopilot is engaged If the Autopilot is engaged the Bank Angle roll angle limit advances to 33 degrees from 50 degrees This input discrete should be connected to a 28V active engaged output discrete from the Autopilot system that indicates the Autopilot has authority over the controls of the aircraft For aircraft with Touch Control Steering the input should be connected to the clutch engaged output discrete Discrete Position Status Connector Pin Autopilot Engaged Engaged 28V Not Engaged Open J1 8 3 15 1 9 Terrain Awareness and Inhibit Discrete The Terrain Awareness and TCF Inhibit discrete inhibits the Terrain Awareness and TCF modes of the MK VINIII EGPWS This discrete is required for all installations that do not disable TA amp D and in Category 6
357. operating the system s If problems are encountered in performing these procedures the installer may refer to aircraft wiring diagrams for harness troubleshooting or the aircraft maintenance manual to isolate faulty equipment All discrepancies should be resolved before proceeding This section will also load the Regional Terrain Database in MK VI EGPWS that will be operating outside the AMERICAS region 4 2 Harness Checkout and Power Check Prior to installing any equipment it is important to verify that all interfaces have been made and that power and ground at each unit connector is correct using the wiring diagrams for the installation Any discrepancies in the wiring must be resolved before proceeding The wire harness should also be checked for proper clearance near any control cables and other potential areas that may cause binding and or chafing 4 3 Unit Installation After the harness check has been completed and any discrepancies have been resolved the units should be installed into their respective racks and all connections to the wiring harness should be made connectors attached Verify that all of the units are secure in their respective racks panels etc and all harness connections are secure Refer to aircraft installation drawings for the unit locations and mounting information 4 4 EGPWC Initialization and Configuration The first time a MK VI MK VIII EGPWS is turned on in a new installation the Configuration Module in
358. ormat 1 with GPWS Inhibit gt Input Output discrete definitions Lamp format 2 X 5 Input Output discrete definitions 020 x x Lamp format 2 Flashing lamps with GPWS Inhibit Input Output discrete definitions Lamp format 1 020 X X with GPWS Inhibit and Mom Steep Approach Select T with GPWS Inhibit and Mom Steep Approach Select x 254 254 Windshear Input Output discrete definitions 020 N A X Lamp Format 1 255 255 Windshear Input Output discrete definitions 020 N A X Lamp Format 2 4 Input Output discrete definitions 020 X X Lamp format 1 Flashing lamps with GPWS Inhibit Input Output discrete definitions 3 Lamp format 2 with GPWS Inhibit 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 258 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 0 Input Output Discrete Type 0 CHANNEL CONN PIN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE J1 38 28V DISC 02 28V Glideslope Inhibit Discrete pe J1 19 GND DISC 02 GND Glideslope Inhibit Discrete ob c m J1 37 28V DISC 03 28V Landing Flaps Discrete 2 n J1 18 GND DISC 03 GND Landing Flaps Discrete 2 J1 36 28V_DISC_04 28V Audio Inhibit Discrete ge mm Gnd Inhibit J1 17 GND_DISC_04 GND Audio Inhibit Discrete 6 6 16 lt not gt Gnd Not Inhibit so moa onerar runner pants
359. ow Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 The IOC BUS fault will be present only if both MG inputs have failed 3 The Honeywell EFIS SG amp MG provide Terrain display relay control 4 The EGPWS ARINC 429 Output Bus must be connected to the display 5 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGPWS Self Test 6 Display channels 1 and 2 are multiplexed on ARINC 453 bus 1 7 This display uses the following ARINC 429 labels from the EGPWS for annunciations Label 050 Ifbits 11 14 left range output from the EGPWS does not match left MFD range via label 171 then display white RANGE MISMATCH on the left PFD and MFD Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 232 8 Label 051 Honeywell MK VI MK VIII EGPWS Installation Design Guide If bits 15 18 right range output from the EGPWS does not match right MFD range via label 171 then display white RANGE MISMATCH on the right PFD and MFD If bit 17 1 then display white TERRAIN OFF message on PFD and MFD Labels 05
360. ow Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the SPZ8000 display Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 240 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 7 Category 7 Options Select Group 1 The following table provides identification of the Options Select Group 1 Each entry in the ID column corresponds to a particular combination of TA amp D Alternate Pop Up Obstacle Awareness Enabled Peaks Mode Enabled Bank Angle Enable Steep Approach Enabled Flap Reversal and GPS Altitude Reference selection Refer to section 7 5 for configuration messages that will be present for each option selected Table 5 3 7 Options Select Group 1 Steep TA amp D Peaks Obstacle Bank Angle Flap GPS Altitude Software Approach Alternate Mode Awareness Enable Reference Effectivity Enabled Pop Up Enabled Enabled False False False False False False False Fase True WGS M 420 False False False False False False False False False Tme Ine 00 False False True False False WGS 84 020 False False Tre False False 020 False False False False True True Tre False False False False False False False False True L Ime Ime wosst 00 _
361. ower up The configuration is copied into Non Volatile Memory NVM of the EGPWS The Configuration Module is programmable via an RS 232 interface with the EGPWS The contents of the Configuration Module can also be read back via the same RS 232 interface An optional Configuration Module is available under P N 700 1710 001 for non Internal GPS operation only The 700 1710 020 Configuration Module includes a GPS Real Time Clock RTC counter and position memory to aid in GPS initialization A capacitor will keep the position memory retained and clock current for Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 15 Honeywell MK VI MK VIII EGPWS Installation Design Guide approximately 35 days GPS initialization time should be less than 3 minutes with active RTC data If the capacitor has discharged then GPS initialization time may be as long as 10 minutes 1 5 4 GPS Antenna and Cabling EGPWS installations using the internal GPS require a GPS antenna and cabling The GPS antenna should meet the following qualifications Frequency 1575 42 MHz Impedance 50 ohms Gain 33 dB max 26 5 dB preferred Power 5 VDC Qualification TSO C129 C129a or C144 Antenna gain is limited to 33dB gain maximum Antennas with 26dB gain are preferred There are Active GPS antennas with higher gain However as the active antenna amplifiers amplify noise as well as the signal this can overdr
362. physical discrete and the 429 discrete word bit if configured by the display type Proprietary notice on title page applies CAGE CODE 97896 SCALE SIZE A DWG 060 4314 150 REV SHEET 266 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 13 254 Input Output Discrete Type 254 CHANNEL CONN PIN DESIGNATION PIN TYPE PIN FUNCTION Polarity Configuration REFERENCE J1 38 28V DISC 02 28V Glideslope Inhibit Discrete 6 6 12 Inhibit lt 4 4V Not Inhibit mpm Gnd Inhibit J1 19 GND_DISC_02 GND Glideslope Inhibit Discrete 6 6 11 lt not gt Gnd Not Inhibit 28V Landing Flaps Discrete gt 17V Flaps Up SEAT DISD 103 Flap Override Switch non momentary lt 4 4V Not Flaps Up E GND Landing Flaps Discrete Gnd Flaps Up 18 SND Disk Flap Override Switch non momentary lt not gt Gnd Not Flaps Up gt 17V Inhibit J1 36 28V_DISC_04 28V Audio Inhibit Discrete 6 6 17 44 AV Not Inhibit iie TNI Gnd Inhibit J1 17 GND_DISC_04 GND Audio Inhibit Discrete 6 6 16 lt not gt Gnd Not Inhibit 6 5 6 4 6 3 6 2 6 7 U is pere ows ROMER ds woxours owu GPWS Warning Discrete 7 4 1 J1 78 DISC_OUT_1 Output Terrain Awareness Caution or Warning 7 4 7 1 Obstacle Awareness Caution or Warning 7 4 7 2 J1 77 DISC_OUT_2 Output GPWS Alert Discrete Glideslope Only a J1 76 DISC_OUT_3 Output Glideslope Ca
363. pit Self Test if inhibited Level 6 Audio readout Inhibit gt Terrain Off Terrain Awareness amp TCF Inhibit Not Inhibit gt Terrain On 6 6 21 Autopilot Engaged Discrete 1 An Autopilot Engaged Discrete may be used by EGPWS for the Bank Angle mode computation Type Discrete from the Autopilot system Signal Status Engaged or Not Engaged Level 6 Audio readout Engaged gt Autopilot On Not Engaged gt Autopilot Off Autopilot Engaged Discrete 6 6 22 Barometric Altitude Validity Discrete A Barometric Altitude Validity Discretes may be used by EGPWS for the barometric rate sensor Type Validity from barometric altitude sensor Signal Status Valid or Invalid Level 6 Audio readout e 1 Valid gt Altitude Valid Barometric Altitude Validity Discrete Invalid Altitude Invalid 6 6 23 Magnetic Heading Validity Discrete A Magnetic Heading Validity Discrete may be used by EGP WS for the Mag Heading sensor Type Validity from Magnetic Heading sensor Signal Status Valid or Invalid Level 6 Audio readout T Valid gt Magnetic Heading Valid Magnetic Heading Validity Discrete Invalid gt Magnetic Heading Invalid 6 6 24 Attitude Validity Discrete A Attitude Validity Discretes may be used by EGPWS for the Pitch and Roll signals Type Validity from vertical gyro or attitude computer Signal Status Valid or Invalid Level 6 Audio readout V
364. po Decet neuer 68 3 74 Audio Menu Selection si e IRR EE PR OR MU 66 THSIPUGHOTIS ee eere poen testen le esee con 68 3 0 CATEGORY 6 TERRAIN DISPLAY SELECT 0 2 25 csccsedddscisescescosteccudbvebscheviaiediceseotcscosbicendisevecheviaitdacuseotovcesaecentusette 69 3 81 TDCESelection inulta uerbi dede e hua a u ns 69 3 6 2 Terrain Display Configuration Group sees nete 70 3 8 3 Display Control Group ec RE RE E e Re te Oe eret de 70 3 84 Output 429 BUS GOUD EET 71 DOs JIRSIFACIOTIS 1er 71 3 6 6 Sample Display Sehemati s l atau a hadiah A aaah aa waw ua i 71 3 9 CATEGORY 7 OPTIONS SELECT GROUP 88 3 9 L Steep ADDroUCh cron n a e Z e A ER d a D L iet e 88 3 9 2 FAKD Aliernale POP UP iei ay FRENAR TR 88 3923 PCOKS MO unte HEAT Seah Sd re ret ETRE 88 3 9 4 Obstacle MWarenessczi tse te an OS 88 3 9 3 Bank Angle Callout Enabling n eda ep idest ertet eris ese ta 89 3 9 0 Flap Reversa e ier p de adde itt aa aa 89 3 9 7 GPS Altitude Reference unn h e d eta n teu aN u esee ened 89 3 9 6 eee bee
365. power The 78 pin is a Subminiature D High Density Series connector conforming to Mil C 24308 The 50 pin is a Subminiature D Connector conforming to Mil C 24308 78 pin Connector Vendor Supplier Supplier P N Honeywell P N DD78F10JVLC 15 440 1158 009 P2 50 pin Connector Vendor Supplier Supplier P N Honeywell P N RD5OFIOJVLC 15 440 1233 001 A GPS Antenna connector is required for Enhanced MK VI and MK VIII units with internal GPS receiver GPS Connector Vendor Supplier Supplier P N Honeywell P N 225554 6 440 1239 001 For a pictoral of the front panel connectors see Figure 8 1 1 and 8 1 2 Also refer to Section 8 for pin out information A test connector J3 is provided on the EGPWC front panel This provides access for a PC test monitor and future portable data loading capabilities The mating connector for the EGPWC test plug is a male pins 15 pin double density D subminiature type Positronics Industries kit part number ODD15M1OYOZ or the following individual parts Backshell Shielded Cable Clamp Assembly 74845 The following tools will work with Positronics Amp and Mil Spec Connectors Insertion Extraction Tool 91067 1 M81969 1 04 Hand Crimp Tool 22 M225202 01 M22520 2 09 Positioner Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 160 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 2 3 Configuration Mod
366. pplies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 285 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 2 31 Roll Angle 325 ROLL ANGLE Source ARINC 704 INU IRS AHRS FMS or IOC LABEL Octal 325 Units Degrees 180 Max Range 180 Degrees Approx LSB 0 01099 Deg Data Bits 15 to 28 14 Right Wing Down Sign Bit 29 Pad Bits 11 to 14 Transmit Interval mSec 10 to 36 Data 2 s Complement Binary SDI Bits 9 10 6 2 32 Magnetic Heading 320 MAGNETIC HEADING Source ARINC 704 INU IRS AHRS FMS or IOC LABEL Octal 320 Units Degrees 180 Max Range 180 Degrees Approx LSB 0 00549 Degrees Data Bits 14 to 28 15 Clockwise from North Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 10 to 50 Data 2 s Complement Binar SDI Bits 9 10 6 2 33 Localizer Deviation 173 or 116 Transmit Interval mSec 33 3 to 66 6 Data Type 2 s Complement Binary SDI Bits 9 10 115 ms max for IAC 100 ms max for IOC NOTE Units Difference in Depth of Modulation DDM 0 0775 DDM 1 Dot 6 2 34 Pitch Angle 324 LABEL Octal 271 Units NM Max Range 1023 5 Approx LSB 0 5 6 2 36 DSU Status Word 350 Approx LSB N A Sign Bit N A DSU STATUS WORD BIT ASSIGNMENTS DEFINITION Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 286 Honeywell MK VI MK VIII EGPWS Installa
367. pplies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 170 Honeywell MK VI MK VIII EGPWS Installation Design Guide Connector Type TNC Low Level DC on RF Output 5 VDC 5 50 mAmps maximum Shield Ground Pin Assignment Signal Mnemonic GPS ANT COAX 4 2 10 OAT Voltage Reference Output This output is an accurate voltage source for 500 Q resistive temperature sensors Quantity 1 Output Voltage 5 000 VDC 10 mVDC no load Nominal Load 500 Q Pin Assignment Signal Mnemonic J1 25 OAT REF NOTE This output has a source impedance of 4 42 0 1 4 2 11 Lamp Driver Outputs The MK VI and MK VIII EGPWC support two kinds of Ground Open discrete outputs used to signal various discrete conditions Monitor outputs are used to signal failure conditions for the MK VI and MK VIII EGPWC Monitor outputs default to an active state when there is a failure or if power is removed from the MK VI or MK VIII EGPWC The other Lamp Driver outputs are used to signal the alert or mode control status of the MK VI and MK VIII EGPWS Short term current limit protection is provided on all drivers for output shorting conditions Ground going output discretes may be connected together to produce a wired OR function for the active low state of the signals If output discretes are wired Or d then diodes must be installed for isolation 4 2 11 1 Monitor Output Characteristics Quantity 3 Type of Output Switch Closure to G
368. prevents the EGPWS from reporting an external bus fault on the second channel 6 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGPWS Self Test 7 At the time of this printing this configuration is not supported by Primus 1000 hardware prior to installation contact Honeywell EGPWS group for applicability Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 221 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 239 Collins FPI 9XX Integrated with binary Peaks MK VIII Only Display Configuration Group 244 Display Type Collins FPI 9xx with binary Peaks Elevations F tet Sweep Type Auto Pop Up 5 3 7 therefore enable disable of pop up is done via the display Peaks Mode Binary Peaks Elevations Yes Data passed by ARINC 429 Labels 011 and 012 Manual Select Selection is controlled by display Display bus type DISPLAY BUS 1 CONNECT TO 453 1 1 58 Terrain Display data to switching relay Symbol Generator 1 4 2 13 2 B J1 59 7 2 DISPLAY BUS 2 CONNECT TO 453TX 2 J1 56 Terrain Display data to switching relay Symbol Generator 2 4 2 13 2 B J1 57 7 2 Display Input Control Group 253 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2
369. provides identification of the Altitude Callouts Menu Each entry in the ID column corresponds to a particular menu selection The Altitude Callouts menu ID s 0 through 12 consist of standard callouts Selecting ID 0 12 will result in the callouts listed being enunciated Smart 500 activation is reflected by a 500 callout being spoken at the end of the selected callout menu sequence in the Long Level 1 Self Test In addition the Callout menu ID number and the Smart Callout Selected configuration message will both be given during level 3 Self Test and in the RS232 Present Status display Table 5 3 4 Altitude Callouts Smart Software Callout Effectivity Selected True 020 True 020 MINIMUMS MINIMUMS 50 40 30 20 10 True 020 True 020 020 False False 020 x x x gt lt gt gt MINIMUMS MINIMU gt gt x MS m x x MINIMUMS x 020 gt gt gt gt False 020 020 020 False x alse x alse B 1 Compliance with TSO C151a requires a 500 callout These IDs cannot be used on installations requiring compliance with TSO C151a unless there is an alternate source of the 500 callout 2 This ID provides Above Field Callout Geometric altitude and runway database are used to calculate the height above field If this ID i
370. ption was available see the Effectivity entry Appendix E Tables 5 3 11 x where x is the Heading Input Select number define the format and electrical interfaces required to support each Heading Input Select Type 3 13 1 Magnetic Heading Magnetic Heading is used for Terrain Awareness alert and display 3 13 2 Analog Heading Synchro Cat 11 ID 0 EGPWS MK VI MK VIII J1 Directional Gyro 22 X X Heading Synchro lt Y 23 M Y Heading 2 3 5 Z Z H 4 HG H 26 VAC Reference Heading Ref 24 o C Mag Hdg Validity 28 28V Valid Analog HDG vsd Vendor Model Heading Heading Reference Heading Synchro Note 1 Directional Gyro Valid H C X Y Z Aeronetics Model 9100 P1 28 P1 6 P1 7 P1 8 P1 9 P1 10 Collins 332E 4 P1 F P1 D P1 E P1 A P1 B P1 C Collins AHC 85 P1 9 P2 57 P2 58 P2 34 P2 35 P2 36 Collins DGS 65 P1 50 P1 6 P1 3 P1 25 P1 40 P1 24 Honeywell HG1075 1095 J1B G2 J1B F13 J1B G13 J1B E10 J1B E11 J1B E12 Honeywell KSG 105 P1 V P1 P P1 D 1 2 P1 w 1 P1 C P1 F P1 T 1 P1 K Honeywell 525 KG 102 J2 P J2 R J2 U J2 S J2 V J2 T JET DN 104 P2 31 P2 9 P2 10 P2 1 P2 2 P2 3 Litef LTR 81 MP E15 MP B12 MP B13 MP B9 MP B10 MP B11 Litef LCR 92 LCR 93 Note 2 J3 05 J3 20 J3 13 J3 42 J3 28 Sperry C 14A 1 1 P1 J P1 L P1 M P1 K Sperry C 14D P1 DD P1 X P1 Y P1 AA P1 BB P1 Z Sperry DG 23
371. put 429 Bus Group 1 Channel Pins Comments 429TX_1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x and 7 1 5 x B J2 42 429 2 Low Speed A J2 26 Transmits Section 7 Label sets 7 1 1 7 1 2 x 7 1 3 x 7 1 4 x and 7 1 5 x B J2 9 Integration Notes When interfacing to a single display controller configuration the bus must be connected to both EGP WS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 219 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 237 Honeywell Primus 1000 with binary Peaks Elevations and Cyan MK VIII Only ASCII window text Display Configuration Group 242 Display Type Honeywell Primus 1000 with binary Peaks Elevations Sweep Type 5 3 7 Alternate Pop Up False TA amp D Alternate Pop Up True Pop Up On Caution or Warning Never Pop Up Peaks Mode Category 7 Options Select Group 1 Peaks Enable False Peaks Enable True Manual select Selection is controlled by display Deselection is controlled by displa n Yes Data passed by ARINC 429 Labels 011 and 012 221 Yes 10NM C a Moving Marker Yes Honeywell type Yes for Peaks Elevations only located middle right side of display
372. put A leg i en IOC 2 ARINC 429 Input A leg J2 42 429TX 1B EGPWS ARINC 429 Output 1 B leg J2 43 429TX 1A EGPWS ARINC 429 Output 1 A leg J2 44 ADC TXB RS 422 Transmit B leg port 2 J2 45 GPS TXA GPS RS 232 Transmit port 3 RS 422 Transmit A leg port 3 J2 46 GPS TXB RS 422 Transmit B leg port 3 J2 47 i own I I _ o S 5 Reserved ____ _____ 13 12 13 13 13 14 3845 Reserved 7 O GPS ANT COAX GPS COAX connection Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 321 Honeywell MK VI MK VIII EGPWS Installation Design Guide Figure 8 1 1 Front Panel Connector Orientation J1 J2 J3 GPS ANT Note The GPS ANT connector only applies to the 965 1190 0xx and the 965 1220 0xx MK VI EGPWS shown HARO WARE MOO STATUS 1 56 2 z ino 011 5e 20 5 13 T 6 T39 E101u CLAS THEKI DU2r BPE SOFTWARE 050 1768 LEVEL C D ENVIR DAT 00 1600 WTiS 2LB MAX DATABASE Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 322 Honeywell MK VI MK VIII EGPWS Installation Design Guide Figure 8 1 2 Connector Pin References J1 J2 J3 J3 JOC 55 8 amp
373. quired Data used if present Table 5 3 3 253 Position Input Type 253 Dual High Speed ARINC 743A GPS CHANNEL CONNECT TO IOC 1 ARINC 743A 2 Fault Designation IOC BUS 1 429RX 1 Format ARINC 429 High Speed Bus Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 000 Longitude Normal 6 2 8 20 180 Degrees Basic 0 00017166137695 000 Latitude Fine 6 2 59 1 0 000172 Basic 0 00000008381903 000 Longitude Fine 6 2 60 0 000172 Basic 0 00000008381903 000 Vertical Velocity 6 2 58 32768 Basic 1 000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 000 Altitude 6 2 4 131 072 ft Basic 0 125 000 VFOM 6 2 13 32768 ft Basic 0 125 000 HFOM 6 2 10 16 Basic 0 000061035 000 Ground Speed 6 2 6 4096 Knots Basic 0 125 000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 000 Sensor Status 6 2 16 Discrete Wd Basic n a 000 UTC 6 2 17 Discrete Wd Basic 0 1 min 000 Date 6 2 18 Discrete Wd Basic 1 day 000 n N NO NO QA tA CHANNEL CONNECT TO IOC 2 ARINC 743 2 Fault Designation IOC BUS 2 429RX 3 Format ARINC 429 High Speed Bus Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 000 Longitude Normal 6 2 8 20 180 Degrees Basic 0 00017166137695 000 Latitude Fine 6 2 59 1 0
374. r directly but can also be used to drive other devices with equal or higher impedance Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 171 Honeywell MK VI MK VIII EGPWS Installation Design Guide Quantity 1 Maximum Power Output 4 Watts Nominal Nominal Output Impedance 8Q Load Impedance 8Q or greater Number of Available Power Output Levels 5 selectable levels excluding the Mode 6 Audio Reduction function Pin Assignment Signal Mnemonic Signal J1 70 Return J1 71 4 2 12 2 Low Level Interphone Audio Output The 600 ohm output is capable of driving one 600 ohm load at the specified level or at a reduced level This output is primarily designed for headphones and interphone systems Quantity 1 Nominal Output Impedance 6000 10 Maximum Single Channel Power Output 100 mW Nominal Available Power Output Levels 5 selectable levels excluding the Mode 6 Audio Reduction function Pin Assignment Signal Mnemonic Signal J1 75 Return 1 74 4 2 13 ARINC Digital Serial Output Buses 4 2 13 1 ARINC 429 Output Bus The ARINC 429 output buses are defined in the terrain display select Section 5 3 6 3 output 429 bus group AUD HL H AUD HL D AUD LL H AUD LL L Quantity Format Low Speed Data Rate High Speed Data Rate Direction of Information Flow Word Frame Structure Data definition Pin Assignment Signal Mnemonic Bus 1 A leg Bus 1 B l
375. r isolation Output discretes are intended to operate with 28 VDC lamp sources and will not operate with 5 VDC lamp sources 3 15 2 1 Lamp Format The Lamp Format Type configuration is a function of the discrete output pin functions and defines the operation of the red and amber GPWS cockpit lamps For Lamp Format 1 the amber Below G S lamp is driven by the GPWS Alert Glideslope only discrete and the red GPWS lamp is driven by the remaining alerts and warnings For Lamp Format 2 the red GPWS lamp is driven by the GPWS Warning Pull Up Terrain Pull Up and Obstacle Pull Up only discrete the amber GPWS lamp is driven by the remaining alerts and warnings Note Lamp Format 2 is highly recommended by Honeywell As of April 2002 the FAA position paper on Lamp Format is in draft form the FAA may require that all new installation of EGPWS use Lamp Format 2 3 15 2 2 Flashing Lamps The Flashing Lamps option is configurable as a function of the discrete output pin functions and defines the operation of the red and amber GPWS cockpit lamps If the Flashing Lamps option is selected both the red and amber GPWS cockpit lamps will flash when they are illuminated if Flashing Lamps is not selected they will be illuminated as steady lights 3 15 2 3 GPWS INOP Discrete The GPWS INOP discrete J1 72 indicates GPWS modes are inoperative This feature activates a GPWS INOP lamp located in the cockp
376. ration 364 MKVIII EGPWS w Windshear only Note Normal Acceleration is corrected by Sine of Body Angle of Attack 7 1 2 14 Computed Flight Path Angle 375 MKVIII EGPWS w Windshear onl 7 1 2 15 Scaled Total Shear 376 MKVIII EGPWS w Windshear onl LABEL Octal 376 Max Range 4 0 g s Approx LSB 0 00012207 g s Data Bits 14 to 28 15 Headwind Updraft Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 100 20 Data Type 2 s Compliment Binary SDI Bits 9 10 Proprietary notice on title page applies CAGE CODE 97896 SCALE SIZE A DWG 060 4314 150 REV SHEET 309 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 3 Terrain Display Outputs The following ARINC 429 outputs support the Terrain Display function 7 1 3 1 Displayed Range 050 Label Octal 050 Transmit Interval 200 msec 10 NO DEFINITION 11 14 TERRAIN DISPLAY RANGE 1 0 5 to 2000 NM format 15 18 TERRAIN DISPLAY RANGE 2 0 5 to 2000 NM format 19 29 UNDEFINED NOTE Bits contain left and right side Terrain Display Ranges 0 5 to 2000 NM format as follows Bits 14 11 amp Bits 18 15 0000 0001 0010 0100 0101 0011 M M 7 1 3 2 Terrain Display Status Word 051 Data Discrete Label Octal 051 Transmit Interval 200 msec 10 BIT DEFINITION 11 POP BOOLEAN 1 12 POP UP BOOLEAN 2 13 TERRAIN DISPLAY VALID
377. re found in Table 5 3 3 0 In this category only the following Position signals are defined Altitude e Sensor Status Date e True Track Angle Ground Speed e Universal Time Correlation Horizontal Figure of Merit HFOM Vertical Figure of Merit VFOM Horizontal Integrity Limit e N S Velocity Latitude Position Velocity Longitude Position e Vertical Velocity used if present Table 5 3 3 Position Input Select Position 220 Software Input Type Effectivity 5 3 3 x L5 i IRC age X X 1 GPS ARINC 429 low speed ARINC 743 format 020 X x 2 2 lt 2 X X gt GPS ARINC 429 high speed ARINC 743A format 020 X X oes ARINC 429 high speed ARINC 743 format ARINC 429 low speed ARINC 743A format ese No N S E W velocities Note 2 GPS ARINC 429 low speed ARINC 743 format x x No N S E W velocities Note 2 GPS ARINC 429 high speed ARINC 743A format x No N S E W velocities Note 2 GPS ARINC 429 high speed ARINC 743 format po No N S E W velocities Note 2 Dual IOC GPS ARINC 429 high speed ARINC 743A 020 format No N S E W velocities Note 2 Dual GPS ARINC 429 high speed ARINC 743A format NOTE 1 The GPS Altitude Reference in Category 7 Options Select Group 1 must be properly applied for the appropriate GPS Position type
378. red when weighing the aircraft for weight and balance If the GPS antenna is tilted more than 5 or is mounted close to other objects that shadow it loss of some of the satellites will occur and system performance degraded See manufacturer for specifications of GPS antennas Some GPS Antenna cable and connector information including vendor information is listed below Cable Length Cable Part EGPWS TNC Antenna TNC Max Loss Number VPN Connector VPN Connector VPN 0 to 40 ft RG142B U TED Mfg 5 10 30 TED Mfg 5 30 102 1 8 0 RG400 U 0 to 80 ft ECS 311601 TED Mfg 5 10 307 TED Mfg 5 10 307 8 0 0 to 100 ft ECS 311201 TED Mfg 5 10 306 TED Mfg 5 10 306 8 0 100 to 165 ft Contact TED ECS or PIC for complete cable connector assembly Maximum Allowable Loss dB 1575 MHz for cable and connector using nominal 26 5 dB gain TED Manufacturing Corp Electronic Cable Specialists ECS PIC Wire amp Cable 11415 Johnson Drive 5300 W Franklin drive N63 W 22619 Main Street Shawnee Kansas 66203 Franklin Wisconsin 53132 Sussex Wisconsin 53089 Tel 913 631 6211 Tel 800 327 9473 Tel 800 742 3191 2 3 7 GPS Antenna Installation Refer to manufacturer s procedures or applicable STC documentation 2 3 8 OAT Sensor Location The OAT sensor should be mounted on the underside belly of the aircraft or other convenient location meeting the following conditions Avoid mounting the sensor where it can b
379. rietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 277 Honeywell MK VI MK VIII EGPWS Installation Design Guide B4 B 000 001 010 011 100 101 110 111 Aoh 1 p K OM L 1 1 o 1 lt gt BOX M j SER 1 1 l gt N t TRI t MOND 6 2 1 Uncorrected Barometric Altitude 203 UNCORRECTED BAROMETRIC ALTITUDE Source ARINC 706 DADC or IOC LABEL Octal 203 Max Range 131 072 Feet Approx LSB 1 Foot Data Bits 12 to 28 17 Above Sea Level ASL Sign Bit 29 Pad Bits 11 Transmit Interval mSec 31 3 to 62 5 Data Type 2 s Complement Binary SDI Bits 9 10 50 if DAU 6 2 2 Static Air Temperature 213 Units Degrees Celsius Transmit Interval mSec 250 to 500 SDI Bits 9 10 6 2 3 Barometric Altitude Rate 212 Approx LSB 16 Ft Min 6 2 4 Altitude 076 GPS MSL Units Feet Approx LSB 0 125 Foot 6 2 5 Horizontal Integrity Limit 130 GPS BIT ASSIGNMENT GPS HIL 11 Set to 1 whenever the receivers detects a non isolatable 28 6 2 6 Ground Speed 112 GPS Ground Speed GPS Source ARINC 743 A GPSSU LABEL Octal 112 Max Range 4 096 Knots Approx LSB 0 125 Knot o DEGREE lt SYMBOL po Toe Data Bits 14 to 28 15 Sign Bit 29 Pad Bits 11 to 13 Transmit Interval
380. rmal gt Glideslope Enabled Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 299 Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 6 14 Decision Height Discrete Type Decision Height Bug switch Signal Status Less than Decision Height or Greater than Decision Height Level 6 Audio readout DH Di t Less Than DH gt Below DH Greater Than DH gt Above DH 6 6 15 Mode 6 Low Volume Discrete Type Mode 6 low volume select switch Signal Status Low Volume Select or Normal Volume Low Volume in this case refers to the 6db volume level used during Self Test Normal Volume refers to the audio output level selected per Category 14 5 3 14 Level 6 Audio readout f Low Volume gt Mode 6 Low Volume Mode 6 Low Volume Discrete Normal gt Mode 6 Normal Volume 6 6 16 GND Audio Inhibit Discrete Type Analog discrete input from a flight deck mounted switch Signal Status Audio Suppress enabled or disabled All Modes Inhibit enable or disable Fault Monitoring Activation of this input will result in the External EGPWS Inhibited Level 6 Audio readout M Inhibit gt Audio Inhibit Not Inhibit gt Audio Not Inhibit 6 6 17 28V Audio Inhibit Discrete Type Analog discrete input from a flight deck mounted switch Signal Status Audio Suppress enabled or disabled All Modes I
381. rminal 2 approach 3 oceanic Error Status true if set false otherwise not used ROM failure RAM failure Nonvolatile RAM lost RF failure not used not used BaseBand ASIC failure BaseBand ASIC timeout 9 not used 10 RS 232 channel 1 receiver timeout 11 EEPROM failure 12 RS 232 channel 2 fail _ 13 1 millisecond underflow 14 not used 15 1 millisecond overflow 6 5 Digital Data RS 422 The MK VI and MK VIII EGPWC supports up to 3 RS 422 digital receivers with 2 receivers having transmit capability also used to monitor broadcast data from other LRUs and to support interactive protocols Each receiver channel follows the characteristics of reference document EJA 422 Transmission System Interconnect Each RS 422 receiver shall be connected to an RS 422 transmitter by means of a single twisted and shielded pair of wires The shield shall be grounded at both ends and at all production breaks in the cable to an aircraft ground close to the rack connector Receiver Bus Frequency Receivers are capable of operating up to 38 4K baud and are determined by configuration selection 6 5 1 Honeywell RS 422 Serial Control Interface SCI Mode Range Word The Serial Control Interface is transmitted on an RS 422 data bus The data stream consists of 13 words a label byte followed by two data bytes transmitted within 47 milliseconds Each character consists of one bit Low 8 data bits with least significant b
382. roduction The Honeywell MK VI MK VIII Enhanced Ground Proximity Warning System MK VI MK VIII EGPWS provides alerts and warnings to prevent controlled flight into terrain CFIT This Installation Design Guide must be used in conjunction with the Interface Description Document Appendix E for the MK VI MK VIII Enhanced Ground Proximity Warning System MK VI MK VIII EGPWS to select features and design the installation for this system It is assumed that the user of this document is familiar with avionics installation practices and aircraft systems associated with the installation and operation of the MK VI MK VIII EGPWS It also assumes access to pertinent aircraft wiring diagrams modification records and manuals The information contained herein together with general procedures outlined in FAA AC 43 13 must be followed carefully to assure a safe electrically sound certifiable and operational installation The contents of this document are for information and reference only and must not be construed as formal FAA approved work authorization 1 2 Applicability This manual is applicable only to MK VI MK VIII EGPWS computers with the following part numbers MK VI 965 1180 020 965 1190 020 MK VIII 965 1210 020 965 1220 020 Part numbers 965 1190 xxx and 965 1220 xxx include an internal GPS card 1 3 How To Use This Document Section 1 provides a system overview Section 2 provides mechanical installation and location
383. round Max Open Circuit Voltage 30 VDC Current Limit 1A Potential Across Closed Switch 2 5 VDC Max Pin Assignment Signal Mnemonic See specific output in Category 13 MON_OUT_xx NOTE Intended to operate with 28VDC lamp sources and will not operate with 5 VDC lamp sources 4 2 11 2 Discrete Output Characteristics Quantity 9 Type of Output Switch Closure to Ground Max Open Circuit Voltage 30 VDC Current Limit 500 mA typical Potential Across Closed Switch 1 VDC Max Pin Assignment Signal Mnemonic See specific output in Category 13 DISC_OUT_xx NOTE Intended to operate with 28VDC pullup external to the EGPWS 4 2 12 Audio Outputs There are two audio outputs provided one 8 ohm output and one 600 ohm output There are several possible volume levels available with the MK VI and MK VIII EGPWS as shown below with maximum output being 4W 8Q or 100mW 6000 The actual audio level output by the EGPWS is dependent on several items e Selection of nominal alert audio volume level max 6 12 18 or 24 dB via Category 14 Section 5 3 14 Jfa soft Glideslope alert is being issued given 6 dB below nominal alert volume level e Ifa Self Test is in progress alerts are given 6 dB below nominal alert volume level e Selection of Mode 6 Low Volume Discrete lowers callout volume by 6 dB See Section 5 3 13 4 2 12 1 High Level Speaker Audio Output The 8 ohm output is capable of driving a speake
384. roup and Output 429 Bus Group are shown in the Appendix E Table 5 3 6 1 x and are used to generate the installation wiring diagrams 3 8 6 Sample Dis play Schematics Honeywell GNS XLs Honeywell Bendix PPI 4B Honeywell KMD 540 550 850 Honeywell Bendix EFS 40 50 Honeywell Grimes TRA 45A Collins WXI 701 711 Honeywell Primus UDI with Avtech DSU Collins Pro Line II IV Honeywell Primus 440 660 880 Integrated Honeywell SPZ8000 SG 802 803 806 Honeywell Primus 1000 Universal MFD 640 Honeywell Bendix RDR 2000 IN182A Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 71 Honeywell MK VI MK VIII EGPWS Installation Design Guide STX SNO PSA L STX SNOD VOINS XXXX 0c0 0967 7 ul SO 0000 8ZS01 900 lenuew uonejejsu S TX SNO II W uolH 295 STX SNO JO uorejedo pue 104 Buunp dn dod ojne jou STX SN9 JO 020 0 21 996 E Jeje JO 020 0 1 L 896 IA MIN TO pi GG ZL 199 gt 5 sng duie1 AgZ 159 A 18 8 INO Z O9pIA 8807 47 199 A 69 9 INO L 8423 47 189 Lr A 0 9 a 8 8 MEO ul z amp ONINV h uz SERT u addy
385. s This light switch may be located in an assembly with the TERR INHIBIT light s and or other EGPWS annunciators TERR INHIBIT ON This light should be located in the flight crew s field of view and within reach of both crew members This light switch may be located in an assembly with the TERR DISPLAY light s and or other EGPWS annunciators Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 42 Honeywell MK VI MK VIII EGPWS Installation Design Guide TERR FAIL This light should be located within at least one crew member s field of view or with other system INOP lights of similar importance Note Annunciators are available with split legend GPWS FAIL TERR FAIL in one assembly It is recommended that this light not be located in the flight crew s primary field of view The reason being that in the event of a GPWS system failure at the beginning of a flight this light will remain ON until the problem is fixed TERR TERR TERR ON INHB FAIL PULLUP GPWS PULLUP GPWS The above picture is an example of lamp location and does not restrict lamp location or format Figure 2 3 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 43 Honeywell MK VI MK VIII EGPWS Installation Design Guide F 20 ov LV 10 50
386. s selected TA amp D and TCF must be enabled MK VI and MK VIII installations cannot select Category 6 ID 2 Note Selecting an Altitude Callout ID without a minimums callout can be accomplished by leaving the Decision Height DH input discrete open Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 193 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 5 Category 5 Audio Menu Select The Audio Menu Select option consists of sets of voices that are mapped to specific warning mode outputs The Audio Menu tables list the alert warning conditions in order of priority The following table provides identification of the Audio Menu Type Each entry in the Audio Menu Type column has a corresponding table that provides detailed information on the configuration For example the details for Audio Menu Type 0 are found in Table 5 3 5 0 Table 5 3 5 Audio Menu Type ID Audio Menu Type Description Software Table 5 3 5 x Effectivi Table 5 3 5 0 Audio Menu Type 0 Basic ALERT WARNING CONDITION AUDIO MENU NOTES MODE 7 WINDSHEAR WARNING SIREN WINDSHEAR WINDSHEAR WINDSHEAR PULL UP TERRAIN TERRAIN PULL UP TERRAIN TERRAIN 2 2 PULL UP MODE2TERRAIN TERRAIN 142 MODE 6 MINIMUMS SELECTEDCALLOUTS 12 TERRAIN AWARENESS CAUTION CAUTION TERRAIN PAUSE CAUTION TERRAIN 4 MODE 4 TOO LOW TERRAIN TOOLOWTERRAN 1 TCF TOO LOW TERRAIN TOOLOWTERRAN 1 _
387. satisfy EGPWS dual input requirements CONN REFERENCE NAME 7 PINFUNCTION Polarity Configuration Reference Type 1 Momentary J1 32 GND_DISC_12 6 6 18 Display Select Discrete 1 Gnd Display Select Toggle lt not gt Gnd Normal Reference Type 1 Momentary J1 31 GND_DISC_13 6 6 19 Display Select Discrete 2 Gnd Display Select Toggle lt not gt Gnd Normal 3 8 4 Output 429 Bus Group This output bus is commonly connected to EFIS and or EICAS displays and Flight Recorders The output transmits MK VI MK VIII EGPWC alert fault and mode status to other systems Output 429 Bus Group Channel Pins Comments 429TX_1 J2 43 Transmits Label sets Section 7 B J2 42 429TX 2 J2 26 No Connection No Data Output B J2 9 3 8 5 Instruction s Using Appendix E Tables 5 2 5 3 6 and 5 3 6 1 x as described above select the Terrain Display Select Type ID that matches the aircraft configuration feature preferences and version part number being installed Record the ID number for the Terrain Display Select Type from Appendix E Table 5 3 6 under the Ident No heading for Step Category 6 in Appendix E Table 5 2 Record the Display Configuration Group number here gt Note This information is used to determine TA amp D Alternate Pop Up and Peaks Mode availability for Category 7 The electrical interfaces pin outs for the Display Configuration Group Display Input Control G
388. screte GND X 4 4 lt GDisc Flap Override Discrete GND from FLAP OVRD SW Glideslope Manual Cancel Discrete GND x 4 15 Glideslope Cancel Discrete Gnd from GS Cancel Landing Gear Discrete GND Discrete X J 1 16 Landing Gear Discrete GND External GPWC Audio Suppression Discrete GND X 4 7 lt GDisc Audio Inhibit Discrete GND Landing Flap Discrete GND Landing Flaps Discrete GND ILS Backcourse Approach Selected Discrete GND Glideslope Inhibit Discrete GND ILS Frequency Selected Discrete GND ILS Tuned Discrete GND Roll Attitude Synchro Y Synchro lt AC Analog3W2 Roll Attitude Synchro Y Spare Reserved J122 lt ACAnalog3w1 Magnetic Heading Synchro X Spare Reserved J123 lt ACAnalog3w2 Magnetic Heading Synchro Y NEN a TEN Teram Awareness amp TOF Inhibit Discrete GND _ AlitudeCallouts Volume Reduction Discrete GND Mode 6 Low Volume Discrete GND GPWSFapOwerideDisemte OND Override Discrete GND rom FLAP OVRD SW _ ELLE Gear Discrete GND Landing Gear Discrete GND External GPWC Audio Suppression Discrete GND Audi inhibit Discrete 9 Landing Fiap Discrete e0 Landing IS Backeourse Approach Selected Discrete GND Gtidesiope inhibit Discrete GND LS Frequency Selected Discrete GND WS Tuned Discrete teno Landing Flap Logic Inversion Program Pin J1 24 lt AC Analog
389. screte 2000NM Basic N A 100 Status 6 5 1 2 FF Discrete N A Basic N A 100 CONN PIN REFERENCENAME _ PINFUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x J2 42 Integration Notes 1 The display does not use EGPWS ARINC 429 Output Bus 2 The display color palette is not compatible with Terrain in the mode Peaks Elevations are outside of the scan area in Sector Scan mode Terrain will not be allowed to display in these modes 3 When interfacing to a single display controller configuration the bus must be connected to both EGP WS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 225 Table 5 3 6 1 244 Manual select Manual deselect Auto Range Moving Marker Overlay Page Display bus type DISPLAY BUS 1 Honeywell MK VI MK VIII EGPWS Installation Design Guide Honeywell EDZ806 non Integrated with dual SCI r
390. se outputs can drive cockpit lamps or act as discrete inputs to other aircraft systems 7 4 7 1 Terrain Obstacle Caution Terrain and Obstacle Cautions can be configured to activate any of the discrete outputs Depending on configuration the Caution discretes will typically activate either the GPWS Warn Lamp the GPSW Alert Lamp or will drive their own output lamps 7 4 7 2 Terrain Obstacle Warning Terrain and Obstacle Warnings can be configured to activate any of the discrete outputs Depending on configuration the Warning discretes will typically activate either the GPWS Warn Lamp or will drive their own output lamps 7 4 8 Terrain Pop Up The Terrain and Obstacle Caution and Warning are combined Or d on one discrete to make a Terrain Pop Up indication for an integrated display system The Pop Up discrete can be used by a display system to differentiate between a manual selection or one due to a Terrain Obstacle Caution or Warning event 7 4 9 Windshear INOP Monitor Discretes The MK VIII EGPWC also produces an additional discrete monitor output for Windshear This discrete reflects the WINDSHEAR INOP functions The status of this discrete is also contained on an ARINC 429 output word 7 4 10 Windshear Warning The MK VIII EGPWC Windshear Warnings be configured to activate any of the discrete outputs Depending on configuration the Warning discrete will typically drive its own output lamp or provide a discrete output to other
391. should contact Honeywell Product Support 800 813 2099 for information regarding the compatibility of equipment not listed in Section 11 Normal business hours 8 00 AM to 5 00 PM Pacific Time Monday through Friday 5 2 2 Equipment Location The EGPWS and associated indicators annunciators and switches should be clearly visible and within easy reach of the pilot s Refer to Section II of this manual for complete installation information 5 2 3 FAA Requirements The installing agency should contact a local FAA Inspector who will determine whether the installation may be approved by Supplemental Type Certificate STC or by submitting FAA Form 337 with an applicable STC package 5 2 4 Ground Test Honeywell has developed a generic Installation Ground Test Procedure for the MK VI MK VIII EGPWS drawing number 060 4167 158 5 2 5 Flight Manual Revision Honeywell has developed a generic Airplane Flight Manual Supplement for the MK VI MK VIII EGPWS drawing number 060 4199 194 5 2 6 Flight Test Honeywell has developed a generic Flight Test procedure for the MK VI MK VIII EGPWS GA Fast and GA Slow aircraft drawing number 060 4188 041 A separate generic Flight Test procedure has been developed for MK VIII EGPWS Bizjet aircraft drawing number 060 4188 023 The Flight Test procedures were developed for Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 128 Honeywe
392. sic Channel Pins Comments 429TX_1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x B J2 42 429 2 Low Speed J2 26 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x 7 1 4 x 7 1 5 x and 7 1 6 x B J2 9 Integration Notes 1 The EGPWS ARINC 429 Output Bus must be connected to the display 2 Display channels 1 and 2 are multiplexed ARINC 453 Bus 3 This configuration will cause the GPWS INOP TERRAIN INOP and WINDSHEAR INOP lamps to turn on only at the beginning of the EGPWS Self Test 4 This display uses the following ARINC 429 labels from the EGPWS for annunciation s Label 011 012 Upper Lower Peaks Elevations xxx xxx on PFD and MFD Label 050 If bits 11 14 left range output from EGPWS does not match left MFD range via label 171 then display white RANGE MISMATCH on left PFD and MFD Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 234 Label 051 Labels 052 055 Label 274 Honeywell MK VI MK VIII EGPWS Installation Design Guide If bits 15 18 right range output from EGPWS does not match right MFD range via label 171 then display white RANGE MISMATCH on right PFD and MFD If Bit 17 1 then display white TERRAIN OFF message on PFD and MFD and Terrain window will be cleared by EPIC EGPWS ASCII characters are not used Gr
393. sic 0 000061035 000 Ground Speed 6 2 6 4096 Knots Basic 0 125 000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 000 Sensor Status 6 2 16 Discrete Wd Basic n a 000 UTC 6 2 17 Discrete Wd Basic 0 1 min 000 Date 6 2 18 Discrete Wd Basic 1 day 000 Data Reference Sig Bits Range Signal Type Resolution Rate ms Latitude Normal 6 2 7 20 180 Degrees Basic 0 00017166137695 000 Longitude Normal 6 2 8 180 Degrees Basic 0 00017166137695 000 GPS Hor Int Limit 6 2 5 16 nm Basic 0 00012207 000 Altitude 6 2 4 131 072 FT Basic 0 125 000 VFOM 6 2 13 32768 ft Basic 0 125 000 HFOM 6 2 10 16 Basic 0 000061035 000 Ground Speed 6 2 6 4096 Knots Basic 0 125 000 True Track Angle 6 2 9 180 Degrees Basic 0 005493 1640625 000 Sensor Status 6 2 16 Discrete Wd Basic n a 000 UTC 6 2 17 Discrete Wd Basic 0 1 min 000 Date 6 2 18 Discrete Wd Basic 1 day 000 Slowest acceptable update rate in milliseconds This label is not required Data used if present NOTE This configuration may not be selected if an AHRS configuration is required for Attitude and Heading information refer to Category 10 type 1 and Category 11 type 1 due to the conflict with Channel 429 RX 7 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 192 Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 3 4 Category 4 Altitude Callouts The following table
394. sic N A 100 CONNPIN REFERENCENAME __ PIN FUNCTION GND_DISC_12 Reference Display Select Discrete 1 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x J2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel 2 Bendix PPI 4B with blue water capability required for Peaks display Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 203 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 5 Collins ProLine II 5x6 Display Configuration Group Collins ProLine II 5 6 EE Sweep Type Standard with 60 degree limit YV l Auto Pop Up 5 37 Peaks Mode Category 7 Options Select Group 1 Manual select Anytime Manual deselect Anytime Auto Ranse 914 Moving Marker G i G i E Overlay Page s TERR or Peaks Elevations located on upper left
395. side of Terrain f eus Display bus type ARINC 453 o DISPLAY BUS 1 CONNECT TO 453TX 1 A J1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 _ MEN 0 4 NI DISPLAY BUS 72 CONNECT TO PI l SI MEN MENU RE EE J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 Bun Sr uu Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms B J2 40 Range Display Word 2 2 20 271 Discrete 5 320NM Basic N A 100 CONN PIN REFERENCE NAME PN FUNCTION Polarity Configuration J1 32 GND_DISC_12 Reference Display Select Discrete 1 Type 1 Momentary 4 2 7 Gnd Display Select Toggle 6 6 18 lt not gt Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 When interfacing to a singl
396. signal ground lt 120 uA 400 Hz 10 50V between input legs 50V from any leg to signal ground None 0 5 VAC J1 4 J1 24 J2 34 J2 35 26REF 26REF 11 26REF 2H 26REF 2L DWG NO 060 4314 150 REV SHEET 167 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 2 5 ARINC 429 575 Digital Serial Bus Inputs Quantity 8 Format DITS ARINC 429 575 Low or high speed Low Speed Data Rate 12 0 KBPS to 14 5 KBPS High Speed Data Rate 100 KBPS 1 Direction of Information Flow Type A broadcast for ARINC 429 575 Word Frame Structure Type B 32 bit words consisting of 8 bits label and 24 bits data status Data definition Refer to Section 6 of this document Channel Pin Assignment Signal Mnemonic Receive 1 A leg J2 37 429 422RX_1A Receive 1 B leg J2 36 429 422RX_1B Receive 2 A leg J2 39 429RX 2A Receive 2 B leg J2 38 429RX 2B Receive 3 A leg J2 41 429RX_3A Receive 3 B leg J2 40 429RX 3B Receive 4 A leg J2 25 429RX 4A Receive 4 B leg J2 8 429RX 4B Receive 5 A leg J2 21 429RX 5A Receive 5 B leg J2 4 429RX 5B Receive 6 A leg J2 22 429RX 6A Receive 6 B leg J2 5 429RX 6B Receive 77 A leg J2 23 429RX 7A Receive 7 B leg J2 6 429RX 7B Receive 8 A leg J2 24 429RX 8A Receive 8 B leg J2 7 429RX 8B SSM SDI Definition Refer to Section 6 2 of this document 4 2 6 RS 232 RS 422 Digital Serial Bus Inputs Two full duplex RS 232 RS 422 buses and a third
397. sired Attitude signal type Using Table 5 3 11 and any sub tables contained within locate the desired Magnetic Heading signal type Using Table 5 3 12 select 0 NoWindshear unless you are an OEM with a defined aircraft windshear type Proprietary notice on title page applies CAGE CODE 97896 DWG NO Table 5 2 Category ID Selection Procedure Record the Ident ID No on the space available on Ident column of this table Record t he Ident ID No on the space available on Ident column of this table Record t he Ident ID No on the space available on Ident column of this table Record t he Ident ID No on the space available on Ident column of this table Record the Ident ID No on the space available on Ident column of this table Record the Ident ID No on the space available on Ident column of this table Record the Ident ID No on the space available on Ident column of this table Record the Ident ID No on the space available on Ident column of this table Record t he Ident ID No on the space available on Ident column of this table Record he Ident ID No on the space available on Ident column of this table Record t he Ident ID No on the space available on Ident column of this table Record t he Ident 0 ID No on the space available on Ident column of this table 060 4314 150 SHEET 175 Honeywell MK VI
398. splay controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 207 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 9 Honeywell Bendix EFIS 40 50 Non Integrated Display Configuration Group 7 Display Type Bendix EFIS 40 50 Non Integrated fe _ Sweep range 60 degrees Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Pop Up when display is in the Never Pop Up proper mode Peaks Mode Category 7 Options Select Group 1 Elevations via overlay Peaks Enabled False Peaks Enabled True Peaks Off Manual select Overlay Page Yes TERR at middle right of the display Peaks Elevations located middle right of display Display bus type ARINC 453 Po DISPLAY BUS 1 CONNECT TO 453TX 1 J1 58 Terrain Display data to switching relay Symbol Generator 4 2 13 2 B J1 59 7 2 DISPLAY BUS 2 CONNECT TO 453 2 A J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 1 57 7 2 Display Input Control Group 2 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic Data Reference Sig Bits Range Sig
399. splayed source provided on label 163 Note 2 ID 251 252 253 and 255 may only be used in conjunction with other IOC bus selections for categories 2 6 8 10 11 and 12 250 Digital Glideslope Localizer PFD Word and Selected 020 N Course ARINC 429 via dual IOC buses Note 1 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 248 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 9 0 Navigation Inputs Select 0 SIGNAL CONNECTION REFERENCE SUMMARY DATA Format ARINC 547 with Validity Flag amp ILS Select 1 65 Input Basic J1 46 Fault Designation GLIDESLOPE FAULT Validity Glideslope Validity Discrete 1 28V PIN FUNCTION CONNECTION PIN TYPE CHANNEL DESIGNATION Polarity Configuration Reference REFERENCE Glideslope Deviation Discrete 1 lt 4 4V Not Valid 4 2 7 28V ILS Tuned J1 39 Input 28V_DISC_01 gt 17V ILS Tuned 6 6 9 Discrete 1 lt 4 4V ILS Not Tuned 4 2 7 GND ILS Tuned J1 20 Input GND_DISC_01 Gnd ILS Tuned 6 6 8 Discrete 1 not Gnd ILS Not Tuned 4 2 7 Table 5 3 9 1 Navigation Inputs Select 1 CONNECTION Format ARINC 547 with Low Level Validity amp ILS Select 1 65 Input Basic J1 46 Fault Designation GLIDESLOPE FAULT Validity Low Level Glideslope Deviation Validity Format DC Input Type Basic Fault Designation GLIDESLOPE LOW LEVEL VALIDI
400. ss by providing the same information as the standard terrain display mode as well as displaying terrain outside of the aircraft envelope and the highest and lowest elevations of terrain displayed Peaks mode displays terrain based on the absolute terrain elevations Note TAD and TCF must be enabled if Peaks mode is enabled The Display Configuration Group Category 6 defines Peaks Mode availability by defining the effects of enabling and disabling the Peaks Mode enable See Appendix E 5 3 6 1 X for definitions Category 7 enables disables Peaks Mode 3 9 4 Obstacle Awareness The Obstacle Awareness feature adds a database of man made obstacles that are at least 100 feet taller than the surrounding terrain and continuously computes obstacle clearance envelopes ahead of the aircraft issuing Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 88 Honeywell MK VI MK VIII EGPWS Installation Design Guide alerts if the boundaries of these envelopes conflict with obstacle elevation data in the obstacle database similar to the Terrain Awareness function Obstacle data is currently available for North America and parts of the Caribbean and Europe Not all obstacles will be contained in the database Category 7 enables Obstacle Awareness if TA amp D is not disabled in Category 6 Note TAD amp TCF must be enabled if Obstacle Awareness is enabled 3 9 5 Bank Angle Callout Enabling
401. ssage Word 3 054 Message Word 4 055 Equipment Identification Equipment Identification Word 377 Fault Summary Words for Proline 4 21 Fault Diagnostic Word 1 350 Fault Diagnostic Word 2 351 Fault Diagnostic Word 3 355 Peak Binary Labels Peaks Upper Elevation 011 Peaks Lower Elevation 012 7 2 ARINC 708A OUTPUT 73 AUDIO OUTPUT 7 4 DISCRETE OUTPUTS 7 4 1 7 4 2 7 4 3 7 4 4 7 4 5 7 4 6 7 4 7 7 4 7 1 7 4 7 2 7 4 8 7 4 9 7 4 10 7 4 11 7 4 12 Ground Proximity Alerts Discrete Lamp Outputs Audio On Discrete Monitor Discretes GPWS amp Terrain INOP or Terrain Not Available Terrain Display Switching Discretes WxR EGPWS Display Select Flap Override Discrete Glideslope Cancel Discrete Terrain Obstacle Awareness Alert Discretes Terrain Obstacle Caution Terrain Obstacle Warning Terrain Pop Up Windshear INOP Monitor Discretes Windshear Warning Windshear Caution Steep Approach Discrete 7 5 SYSTEM CONFIGURATION STATUS 7 5 1 System Status Messages 8 CONNECTOR INTERFACE 8 1 PINOUT FOR FRONT CONNECTORS SORTED BY PIN NUMBER 9 DEFINITIONS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV 308 309 309 309 309 309 309 309 309 310 310 310 311 311 312 312 313 313 313 313 313 314 314 314 315 315 315 315 315 316 316 316 316 316 316 316 316 316 316 316 317 317 317 318 319 319 324 SHEET
402. t and slower jet aircraft Some of the differences between aircraft types are listed below to assist the reader Bizjet Turbofan MK VIII EGPWS only e Uses Commercial GPWS modes with Bizjet optimized Bank Angle callout A Gear stuck down fault will be indicated if the Gear are down and Airspeed exceeds 290 knots A Flap stuck down fault will be indicated if the Flaps are down and Airspeed exceeds 250 knots Uses either a 2000 ft and greater runway database default or a 3500 ft and greater runway database GA Fast Fast Turboprop e Uses classic MK VI GPWS modes e A Gear stuck down fault will be indicated if the Gear are down and Airspeed exceeds 290 knots e Flap stuck down fault will be indicated if the Flaps are down and Airspeed exceeds 250 knots GA Slow Slow Turboprop e Uses classic MK VI GPWS modes e Allows use of Mode 4 Alternate Airspeed Expansion e A Gear stuck down fault will be indicated if the Gear are down and Airspeed exceeds 200 knots e Flap stuck down fault will be indicated if the Flaps are down and Airspeed exceeds 180 knots The gear stuck and flap stuck faults activate the GPWS INOP and are recorded in fault history In addition the Mode 4 Altitude and Airspeed Expansion variables are defined as follows e Mode 4B Altitude are described as follows 150 Mode The voice Low Flaps is intitiated at 150 feet above the ground 170 Mode 4B The voice Low Flaps is intitiated at 17
403. t meet the following requirements e Cable length must be less than 300 feet 91 4 meters e Wire to wire capacitance must not exceed 50 pF foot e Shielded twisted pair with not less than one twist per inch e Impedance of 78 ohms 10 at 1 MHz ARINC 708 WXR e Impedance of 70 ohms 10 at 1 MHz ARINC 453 bus Vendor Name Vendor P N Description QTY UM Pic Wire amp Cable D620224 ARINC 453 cable AR EA Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 20 Honeywell MK VI MK VIII EGPWS Installation Design Guide Pic Wire amp Cable D5102QX Hi Temp Quadraxial A R EA Pic Wire amp Cable D771553 MIL STD 1553 Data Bus AR EA ECS 4122021 ARINC 453 cable 2 shields A R EA ECS 312402 ARINC 453 cable 3 shields A R Emteq D70 022402T 01 ARINC 453 cable EA 17 176 00002 Military Specification EA M83536 6 022M Relay 4PDT Note 1 A R EA M12883 44 01 Relay Socket Note 1 EA Note 1 Recommended in EFS 40 50 Installation Manual 1 9 2 GPS Antenna amp Cable The GPS Antenna amp cable can be ordered from their manufacturers using the following part numbers Vendor Name Vendor P N Description QTY UM Honeywell P N Bendix King 071 01553 0200 KA 92 GPS Antenna 26dB 1 EA 300 1147 001 Comant Cl 405 2 KA 92 GPS Antenna 26dB 1 EA 300 1147 001 Bendix King 050 0331 8 0000 Antenna Installation Kit OPT EA 405 0432 001 Sensor Systems 567 1575 38 56
404. ta types Appendix E Table 5 3 2 defines the Air Data interface options and identifies the first MK VI MK VIII EGPWS version in which the option was available see the Effectivity entry Appendix E Tables 5 3 2 x where x is the Air Data Type number define the electrical interfaces required to support each Air Data Type 3 4 1 Analog Cat 2 ID 0 3 4 11 12 Air Data Type 0 CIC 04077 or equivalent uses Uncorrected Barometric Altitude input scaled from 1500 feet 5 volts to 30 000 feet 15 volts see Appendix E section 6 1 3 Baro Altitude Rate and Computed Airspeed are not required Baro Altitude Valid is standard 28 volt discrete Total Air Temperature is from a dedicated EGPWS 500 ohm probe using 5 volt excitation from the MK VI MK VIII EGPWC Air Data Type 3 ADS 65 or equivalent uses Uncorrected Barometric Altitude input scaled from 1500 feet 0 18 volts to 46 000 feet 5 52 volts zero volts equals zero feet see Appendix E section 6 1 10 Baro Altitude Rate and Computed Airspeed are not required Baro Altitude Valid is standard 28 volt discrete Total Air Temperature is from a dedicated EGPWS 500 ohm probe using 5 volts excitation from the MK VI MK VIII EGPWC Air Data Type 4 CIC 02702 or equivalent uses Uncorrected Barometric Altitude input scaled from 1000 feet 0 244 volts to 40 000 feet 9 756 volts see Appendix E section 6 1 14 Baro Altitude Rate and Computed Airspeed are not required Baro
405. ted to chassis ground internally It is not necessary to tie them both to ground in the aircraft wiring Pin J1 53 was made available to provide a convenient way to supply a ground to external equipment If the OAT probe is not present nothing needs to be tied to J1 53 3 Connect the Smart Cable Honeywell PN 951 0386 001 to the EGPWC J3 connector 4 Turn the Power Supply ON and that the COMPUTER OK LED on the EGPWC front panel is on 5 Insert the PCMCIA card into the Smart Cable PCMCIA card slot NOTE Precautionary notes on the PCMCIA card regarding insertion and or removal while power is applied should be ignored since the EGPWC automatically handles the application and removal of PCMCIA card power 6 While the loading is in progress the INPROG LED on the Smart Card remains ON and the COMPUTER OK LED on the EGPWC is OFF Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 124 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 When loading is complete the XFER COMP LED on the Smart Card turns ON 8 Remove the PCMCIA card from the Smart Card slot 9 After approximately 15 seconds the COMPUTER OK LED comes ON to indicate that the contents of the PCMCIA card were successfully transferred 10 Remove the Smart Card connector from the EGPWC front panel J3 connector 11 To perform the verification of the Terrain Database version go to paragraph 4 6 6 below
406. ternate action switch in the cockpit The recommended label for this switch is GPWS INHIBIT although labeling for this switch should be consistent with existing cockpit nomenclature Activation of this switch for more than 5 seconds will result in a GPWS INOP indication Discrete Position Status Connector Pin GPWS INHIBIT Inhibit Gnd J1 67 Normal Open 3 15 2 Output Discretes The discrete outputs are defined in Appendix E Section 7 4 The MK VI VIII EGPWS supports two kinds of Ground Open discrete outputs used to indicate various conditions Monitor outputs are used to indicate failure conditions for the EGPW system Monitor outputs default to an active state when there is a failure or if power is removed from the EGPWS no connection if the EGPWC is removed from the rack The Discrete Out Lamp driver outputs are used to indicate alert modes GPWS WARN BELOW 65 etc or mode control status FLAP OVRD Terrain Display Select etc of the EGPWS Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 108 Honeywell MK VI MK VIII EGPWS Installation Design Guide Short term current limit protection is provided on all drivers for output shorting conditions Ground going output discretes may be connected together to produce a wired OR function for the active low state of the outputs If output discretes are wire OR d then diodes must be installed fo
407. tes Effectivity 254 Collins ProLine 21 Integrated with binary Peaks Elevations and Partial Compass 020 N A X Raster patch Note 4 255 Honeywell SPZ8000 Integrated older style WXPD with SCI range Note 5 Note 1 For a description of the KCPB features implemented in a particular software release see Appendix B KCPB Phased Implementation in the EGPWS Interface Methodology document 060 4303 000 Note 2 Refer to Rockwell Collins Service Information Letter EFIS 84 85 86 SIL 2 99 Dated March 16 99 or later revision for information describing the requirements to interface an EGPWS to the Collins Pro Line II system equipped with EFIS 84 85 86 Displays and WXR 350 840 700 or TWR 850 Weather Radar systems This SIL provides guidance on the type and use of Collins WXA 1000 video converter required for EGPWS installations where a WXR 350 radar 15 installed in the aircraft Note 3 This configuration 1s applicable to RDR 4B with a mod that makes it capable of displaying blue Note 4 This ID may only be used in conjunction with other IOC bus selections for categories 2 8 9 10 11 and 12 ID s 240 and 254 can be selected for Pro Line 21 display configurations that provide a Partial Compass Raster patch such as a Citation Jet ID 241 can be selected for Pro Line 21 display configurations that provide a Full Compass Raster patch such as a Challenger 300 Note 5 This interface only supports the SG 810 and SG 811 SPZ 8000 Note 6 SG 465 must
408. the EGPWS harness must be programmed to the specific interface configuration for the aircraft This programming is done via RS 232 cable connection between the EGPWC and a PC running the Honeywell WinViews software This interface capability is provided to facilitate diagnostic and configuration functions with the EGPWC during post installation checkout Refer to Appendix C for instructions related to using the WinViews software 4 4 1 RS 232 Com munication with the MK VI VIII EGPWS The MK VI MK VIII EGPWS computer contains software that allows monitoring of its internal parameters for testing purposes without altering its operation The monitoring of these parameter values enables the operator to quickly determine if the EGPWC is using the correct signal and scaling The communication link utilizes the RS 232 communication protocol configured as follows 19200 Baud No Parity 8 Bits and 1 Stop Bit Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 117 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 4 2 EGPWC Front Panel Test Connector The RS 232 interface with the EGPWC is accomplished a test connector provided on the EGPWC front panel J3 This provides access for a PC test monitor and portable data loading capabilities The mating connector for the EGPWC test plug P3 is a male 15 pin double density D subminiature type or equivalent The connection betwee
409. tion Display Type Collins ProLine 21 Integrated with binary peaks elevations and full compass raster patch Sweep Type Fan Mode with 90 degree limit V Y O O Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TA amp D Alternate Pop Up True Category 7 does not affect pop up logic The display controls pop up therefore enable disable of pop up 15 done via the display Peaks Mode Category 7 Options Select Group 1 5 3 7 Peaks Enable False Peaks Enable True Binary Peaks Elevations Yes Data passed by ARINC 429 Labels 011 402 Select Selection is controlled by display Deselect Deselection is controlled by display Auto Range Moving Marker Overlay Page Display bus type ARINC Compatible Format Collins ProLine 21 label 077 Terrain Mode ProLine 21 system outputs Terrain Mode annunciation it does not use Annunciation EGPWS ASCII message DISPLAY BUS 1 CONNECT TO 453 1 A J1 58 Terrain Display data to Primary Flight Display Multi Function display 1 4 2 13 2 B J1 59 DISPLAY BUS 2 CONNECT TO 453TX 2 J1 56 Terrain Display data to Primary Flight Display Multi Function display 2 4 2 13 2 J1 57 7 2 Display Input Control Group 254 CHANNEL CONNECT TO IOC 1 Bus Fault Designation IOC BUS 1 429RX_1 Format ARINC 429 High Speed Bus Basic 2 37 Data Reference Label Sig Bits Range Signal Type
410. tion Design Guide Program Pin D Status Program Pin E Status Unused always 0 6 2 37 True Heading 314 6 2 38 Corrected Barometric Altitude 204 6 2 39 Computed Airspeed 206 6 2 40 True Airspeed 210 Pad 11 to 13 6 2 41 Decision Height 370 IOC Scaling LABEL Octal 370 Units Feet Max Range 8192 FT Approx LSB 0 125 Foot See NOTE 1 Data Bits 13 to 28 16 Above Ground Level AGL Sign Bit 29 Pad Bits 11 12 Transmit Interval mSec 100 to 200 Data Type 2 s Complement Binary SDI Bits 9 10 NOTE 1 Some IOC configurations may only provide positive ranges 0 to 8192 Feet however the EGPWS supports both positive and negative ranges 8192 Feet for all configurations NOTE 2 This label may be provided in a configuration with a single DH input or in conjunction with a selected MDA input For those configurations which provide DH and MDA on separate labels Format 3 applies Format 1 18 0 0 SDI Format 2 is Left SDI used and Format 3 is No SDI 6 2 42 Normal Acceleration 333 NORMAL ACCELERATION Source IOC LABEL Octal 333 Max Range 4 0 g s Approx LSB 0 000977 g s Data Bits 17 to 28 12 Up See NOTE Sign Bit 29 Pad Bits 11 to 16 Transmit Interval mSec 10 to 20 Data Type 2 s Complement Binary SDI Bits 9 10 NOTE Output reads 0 g s nominal when aircraft is on the ground or during unaccelerated flight Proprietary notice on title page applies CAG
411. tions that can only provide low level GS validity is not supported In these cases only ID 1 can be selected Envelope Modulation will still function for those locations which do not require a Localizer input but not for those that require Localizer TABLE 5 3 9 NAVIGATION INPUT SELECT ID Navigation Descrint on Software EGPWS Inputs Select Effectivity Effectivity Table 5 3 9 x MKVI MK VIII Ta Glideslope ARINC 547 with 28V Validity x Analog Glideslope ARINC 547 with Low Level 1 d 020 X Validity 2 Digital Glideslope ARINC 429 ra Digital Glideslope and Localizer ARINC 429 4 Digital KN40 Glideslope and Localizer ARINC 429 25 25 25 25 25 5 Analog Glideslope Localizer ARINC 547 with 020 x 28V Validity Flag i 0 l Digital Glideslope Localizer and Selected Course 020 N A ARINC 429 via dual IOC buses Note 2 2 Digital Glideslope and Localizer Alternate Input 020 N A Channels ARINC 429 via dual IOC buses Note 2 Digital Glideslope and Localizer ARINC 429 via dual IOC buses Note 2 ED nd 4 Digital Glideslope Localizer and PFD Word ARINC 020 5 254 429 via dual IOC buses Note 1 Digital Glideslope and Localizer Alternate Labels ARINC 429 via dual IOC buses Note 2 Note 1 ID 250 and 254 may only be used in conjunction with other IOC bus selections for categories 2 6 8 10 11 and 12 The use of either the left or right source is based on the di
412. tronic com http www sensorantennas com http www shadin com Email sales shadin com http www spirent systems com Email denniss pgaerospace com http www stacoswitch com SHEET 151 Honeywell MK VI MK VIII EGPWS Installation Design Guide West Coast Specialties P O Box 5010 Contact Preston WA 98050 Bruce Maxwell Rep Ph 425 222 3118 206 232 2871 Fax 425 222 3119 Fax 206 232 3174 CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 152 Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX E Interface Description Document Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 153 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table of Contents APPENDIX E INTERFACE DESCRIPTION DOCUMENT 1 INTRODUCTION 11 PART NUMBER 12 PURPOSE 13 SYSTEM OVERVIEW 14 DOCUMENT OVERVIEW 2 REFERENCES 3 MECHANICAL INTERFACE 3 WEIGHT 3 22 SYSTEM INTERFACE COMPONENTS 3 24 EGPWC Mounting 3 2 2 EGPWC Connectors 3 2 3 Configuration Module 3 3 OUTLINE 4 ELECTRICAL INTERFACE 4 INTRODUCTION 42 SIGNAL INTERFACES 4 2 1 Grounds 4 2 1 1 Chassis Ground 4 2 1 DC Ground 4 2 2 Primary Power Input 4 2 3 DC Analog Inputs 4 2 3 1 Radio Altitude 4 2 3 2 Low Level Glideslope 4 2 3 3 Localizer Deviation or Low Level Glideslope Validity 4 2 3 4 Barometric Altitude 4 2 3 5 Outside Air Temperature 4 2 3 6 Configur
413. tude Source Selects a Glideslope and or Localizer Source Selects a Attitude Source Selects a Magnetic Heading Source Selects a Windshear Input Type SCALE NONE SIZE A Using Table 5 3 1 and any sub tables contained within locate the Aircraft Mode Type Using Table 5 3 2 and any sub tables contained within locate the desired Air Data signal type Using Table 5 3 3 and any sub tables contained within locate the desired Position signal type Using Table 5 3 4 and any sub tables contained within locate the desired Altitude Callout Menu Using Table 5 3 5 and any sub tables contained within locate the desired Audio Menu type Audio Menu types 2 amp 3 are designed for Fixed Gear installations Using Table 5 3 6 and any sub tables contained within locate the desired Terrain Display indicator type and range bus type Using Table 5 3 7 and any sub tables contained within select the desired True or False condition for Steep Approach Enabled TA amp D Alternate Pop Up Peaks Mode Enable Obstacle Awareness Enable Bank Angle Enable Flap Reversal Select functions and GPS Altitude Reference type Using Table 5 3 8 and any sub tables contained within locate the desired Radio Altitude signal type Using Table 5 3 9 and any sub tables contained within locate the desired Navigation signal type Using Table 5 3 10 and any sub tables contained within locate the de
414. ule The EGPWS aircraft configuration is programmed into a configuration module installed in the aircraft wiring This configuration module is identified as follows Vendor Supplier Supplier P N Honeywell 700 1710 001 Honeywell 700 1710 020 The configuration module is installed as part of the P2 mating connector backshell and contains reprogrammable memory for configuration storage Configuration module part number 700 1710 020 contains a Real Time Clock RTC circuit that supplies the EGPWS with date and time to allow the internal GPS receiver to determine GPS constellation shift and provide faster satellite signalacquistion and navigation The Configuration module part number 700 1710 020 will only operate with EGPWC hardware part numbers 965 1180 965 1190 965 1210 965 1220 and software versions 020 or later Configuration module part number 700 1710 001 can be used with all EGPWC hardware part numbers and software versions Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 161 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 3 Outline Dimensions of the MK VI and MK VIII EGPWC hardware and their associated mounting rack are given in this section The mounting rack is identical to that of the MK VI GPWC 8 Lt E J i o o LV gt lt 2 E 9 8
415. und when the aircraft is less than approximately 40 knots airspeed approach airspeed varies by aircraft Contact Honeywell EGPWS engineering for assistance in adapting this discrete input design to your aircraft Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 105 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 15 1 5 Glideslope Cancel Discrete The Glideslope Cancel discrete provides the crew with the capability to manually cancel Mode 5 alerts during an approach The Glideslope Cancel latch is automatically reset when the aircraft descends below 30 feet or ascends above 2000 feet or by selecting a non ILS frequency This discrete is typically supplied by a momentary action cockpit Glideslope mode manual inhibit switch typically part of the Glideslope Lamp assembly Below GS Discrete Position Status Connector Pin Glideslope Cancel Cancel Gnd J1 15 Normal Open 3 15 1 6 Momentary Flap Override Discrete The Momentary Flap Override discrete provides the crew with the capability to manually desensitize mode 4 of the EGPWS when the pilot must land with flaps up or partial flaps For Category 1 GA Fast and GA Slow aircraft only the Flap Override will also bias mode 1 by 300 fpm during operations at airports located in terrain where steep or incompatible terrain clearances are involved Honeywell recommends the installation of the momentary
416. uonelle sul jueudinb3 vGr v L L y jo uonejedo pue 104 uonov sng duie1 AgZ 1591 JO 020 0X2 1 896 IIIA J9 JO 020 0 L 1 996 IA AN dONI ureue L 8 V INO O9PIA 8 V INO L O9PIA ddA g V ul Z ONINV g V ul Lit ONINV SMd93 Proprietary notice on title page applies CAGE CODE 97896 DWG 060 4314 150 REV SHEET 74 SCALE NONE SIZE A Honeywell MK VI MK VIII EGPWS Installation Design Guide YXM snug HOALAV PSA Jansnuug sng A8Z jse dwe Joejeg Aejdsiq 9 87 ul dA L L009 ev NSA HO31AV ale jno Yis GIL PAIE vl 9 6 9 Gl L 84l L L 088 0 8 00 099 BuuyyBrq 099 Orr L Z 8 OL S L Gb t 008 1 LL 7 8 OL 9 6 9 6 S Z t ch 8b 6 O OAV 00S 00 16006 006 002 001 06 591995 SNWidd 0891 1009 N d uonejedo pue NSA ees MSC 1009 eu JO pue eoejiejul 104 uonov JO 020 0X
417. ut is 4 watts rms into an 8 ohm load and 100 milli watts rms into a 600 ohm load The audio output level for Mode 6 alerts can be reduced an additional 6 dB by activating the Mode 6 Low Volume discrete of Category 13 3 16 1 Instruction s Using Appendix E Tables 5 2 and 5 3 14 as described above select the Audio Output Level ID number that matches the feature preferences and version part number being installed Record the ID number for the Audio Output Level from Appendix E Table 5 3 14 under the Ident No heading for Step Category 14 in Appendix E Table 5 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 113 Honeywell MK VI MK VIII EGPWS Installation Design Guide H J1 70 L J1 71 8 ohm H J1 75 gt 600 ohm L Jt 74 bowlevelaudio 21 Audio Panel FIGURE 3 16 1 Audio Interface 3 17 Category 15 17 Undefined Input Selects Category 15 17 are undefined input selects at this time Appendix E Table 5 3 15 5 3 16 and 5 3 17 define the Select options and identifies the first MK VI VIII EGPWS version in which the option was available see the Effectivity entry 3 17 1 Undefined Input Select Select ID 0 for all aircraft configurations Input Select options will be added as new installations types are propagated 3 17 2 Instruction s Using Appendix E Table 5 2 5 3 15 5 3 16 and 5 3 17 as described above select the Input Select typ
418. ut will be biased less than 1 VDC J1 30 LCDEV H J1 10 LCDEV L 12 Dots 0 9 VDC Input will be biased less than 15 dots DWG NO 060 4314 150 REV SHEET 165 Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 2 3 4 Barometric Altitude Quantity Input Impedance each leg Reverse Fault Current Input Voltage Range Input Filter Input Type Broken Wire Detect Pin Assignment Signal Mnemonic Signal Return 4 2 3 5 Outside Air Temperature Quantity Input Impedance each leg Reverse Fault Current Input Voltage Range Input Filter Input Type Broken Wire Detect Pin Assignment Signal Mnemonic Signal Return 1 gt 83 lt 200 LA 0 18 VDC to 15 VDC 0 1 Second Low Pass 10 Differential Input will be biased less than 3000 feet J1 62 ALT_H 11 43 ALT L gt 100 lt 200 pA 0 3 VDC to 0 6 VDC 0 1 Second Low Pass 10 Differential Input will be biased less than 80 C 11 63 J1 44 OAT D NOTE For temperature probe voltage reference see section 4 2 10 4 2 3 6 Configuration Defined DC Inputs Quantity Input Impedance each leg Reverse Fault Current Input Voltage Range Input Filter Input Type Broken Wire Detect Pin Assignment Signal Mnemonic 1 Signal 1 Return 2 Signal 2 Return 4 2 4 AC Analog Inputs Unless otherwise specified Input Impedance X leg Input Impedance Y leg Input Imped
419. utput 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 Left Right shift keys on the display not to be used when displaying terrain 2 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 211 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 13 Honeywell P880 660 440 WXPD with SCI range Integrated Display Configuration Group 11 Display Type 7 Honeywell P880 660 440 radar displays Integrated Peaks Mode Category 7 Options Select Group 1 Manual select Anytime 20 OSO Manual deselect Anyime x l Auto Range Noe 14 Moving Marker Yes across bottom of display __ Overlay Page Yes for Peaks Elevations located at lower left of display Display bus type Honeywell picture bus o Auto Pop Up Category 7 Options Select Group 1 5 3 7 TA amp D Alternate Pop Up False TAS amp D Alternate Pop Up True 5 3 7 DISPLAY BUS 1 CONNECT TO 453 1 11 58 71 59 DISPLAY BUS 2 CONNECT TO 453 2 Not supported for this display type IEEE Display
420. utput Level Select Each entry in the ID column corresponds to a particular nominal alert output level selection Max 6 dB 12 dB 18dB and 24dB The nominal output is 4 W rms for the 8 ohm output and 100 mW rms for the 600 ohm output The Audio Output Level can be additionally reduced by 6dB with the Mode 6 Low Volume discrete see Category 13 The output power level will be the nominal maximum output 4W or 100mW reduced by the volume selection from Table 5 3 14 and the Mode 6 Low Volume discrete Table 5 3 14 Audio Output Level Software Effectivity 5 3 15 Category 15 Undefined for this software release The following table provides identification for a future undefined input select category The entry in the following undefined Type corresponds to a table that will provide detailed information on the configuration The details for Undefined Type 0 are not detailed Table 5 3 15 Undefined Type Undefined Type Description Software Effectivity N A 020 X 5 3 16 Category 16 Undefined for this software release The following table provides identification for a future undefined input select category The entry in the following undefined Type corresponds to a table that will provide detailed information on the configuration The details for Undefined Type 0 are not detailed Table 5 3 16 Undefined Type Undefined Description Software Type Effectivity N A 0
421. ve discussion of SSM settings The following table identifies those outputs that are transmitted Note that the outputs are segregated by functional groups Refer to the subsections following the table for specific format information for each output The subsections are in the same order as the table Proprietary notice on title page applies CAGE CODE 97896 SCALE SIZE A DWG NO 060 4314 150 SHEET 303 Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 7 1 1 ARINC 429 DITS OUTPUTS OPERATIONAL OUTPUTS LABEL DESCRIPTION DISCRETEOUTPUT WORDS 270 EGPWS ALERT INDICATION 271 INTERNAL LOGIC BOOLEANS 2 MODE 6 CALLOUT INDICATION 1 273 MODE 6 CALLOUT INDICATION 2 3 5 72 27 00 067 4 7 1 1 5 EGPWS ALERT DISCRETE 2 LAMP OUTPUT WORD 7 1 1 6 EGPWC ALERT DISCRETE 3 INOP INDICATIONS OF THE MK VI AND VIII EGPWC FUNCTIONS __ INTERNAL DATA OUTPUTS The internal data output labels are lowest priority 135 COMPUTED GEOMETRIC ALTITUDE VFOM 164 RADIO ALTITUDE FILTERED BY MK VI AND VIII EGPWC 261 COMPUTED GEOMETRIC ALTITUDE TERRAIN CLEARANCE COMPUTED BY EGPWS 23 7 1 2 7 BODY ANGLE OF ATTACK RIGHT ________ BODY ANGLE OF ATTACK RIGHT VANE 9 224 _ 7 1 2 8__ BODY ANGLE OF ATTACK LEFT ________ BODY ANGLE OF ATTACK LEFT VANE 9 242 7129 CORRECTED AIRSPEED ______________ CORRECTED AI
422. verify regulatory approval of the annunciation devices installed See Appendix D for Vendors A GPWS P TEST BELOW G S P CANCEL switch annunciator assemblies The GPWS annunciator provides visual indication of an EGPWS warning or alert The GPWS annunciator also has a momentary switch that is used to manually initiate EGPWS Self Test Two GPWS annunciators are required for each aircraft one in the direct view of each pilot If the Lamp Format 2 option is selected see 3 15 2 1 this switch annunciator will be labeled PULL UP and annunciated in red The BELOW G S annunciator provides visual indication of an EGPWS glideslope caution The BELOW G S annunciator also has a momentary switch that is used to manually inhibit EGPWS Mode 5 glideslope alerts Two BELOW G S annunciators are required for each aircraft one in the direct view of each pilot If the Lamp Format 2 option is selected see 3 15 2 1 this switch annunciator will be labeled GPWS and annunciated in amber Vendor Name Vendor P N Description QTY West Coast Spec 90 81401 001 GPWS BELOW G S 2 EA West Coast Spec 90 81401 003 GPWS BELOW G S ALT EA West Coast Spec 90 81401 008 GPWS BELOW G S 1 ALT EA West Coast Spec 90 81401 009 GPWS BELOW G S 1 ALT EA STACO 61406 003 GPWS G S CANCEL ALT EA STACO 61406 004 PULL UP GPWS TEST ALT EA STACO 61406 005 GPWS GPWS TEST ALT EA STACO 61406 006 BELOW G S G S CANCEL ALT EA 1 GPWS BELOW G S GPWS FLAP
423. wich 103 00034 Dual element unheated 1 EA Rosemount 102CT2CB 500 ohm 1 EA Rosemount 102AU1AF Single element heated 1 EA Rosemount 102AU1AG Dual element heated 1 EA Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG 060 4314 150 REV SHEET 23 Rosemount 102EH2BH Rosemount 102EH2EB Rosemount 102JE2FG Rosemount 129H 500 Rosemount 129G 500 Dual element heated 1 Dual element heated 1 Triple element heated 1 EA Single element unheated 1 Dual element unheated 1 Honeywell MK VI MK VIII EGPWS Installation Design Guide EA EA EA EA 1 10 Tools Required 1 10 1 Crimping Tool P1 P2 P3 Description UM QTY Vendor Name amp Part Number Hand Crimping Tool EA 1 Positronic Ind 9507 Hand Crimping Tool EA 1 Daniels AFM8 Hand Crimping Tool EA 1 Military M22520 2 1 Hand Crimping Tool EA 1 Astro 61517 1 10 2 Contact Positioner P1 P2 P3 Description UM QTY Vendor Name amp Part Number Contact Positioner Socket P1 EA 1 Positronic Ind 9502 3 Contact Positioner Socket P1 EA 1 Daniels K41 for 22 to 28 AWG Contact Positioner Socket P1 EA 1 Military M22520 2 06 Contact Positioner Socket P2 EA 1 Positronic Ind 9502 5 Contact Positioner Socket P2 EA 1 Daniels K13 1 20 24 AWG Contact Positioner Socket P2 EA 1 Military M22520 2 08 Contact Positioner Pin P3 EA 1 Positronics 9502 4 Contact Positioner Pin P3 EA 1 Daniles K42 22 28 AWG Contact Positioner Pin P3 EA 1 Mil
424. will follow the same pattern e g 421P 7 Other messages that follow the Terrain Database Version can be ignored When ST Level 3 finishes the message Press to Continue is heard If the ST button is not pressed again the ST sequence terminates NOTE If power was connected to the EGPWC per steps B1 through B4 perform shut down per steps 7 and 8 following 8 Turn Power Supply OFF 9 Disconnect Power leads from the EGPWC END OF TEST Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 126 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION V CERTIFICATION Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 127 Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION V CERTIFICATION 5 1 Introduction This section outlines the procedures required to obtain FAA approval for the MK VI MK VIII EGPWS installation Recommended flight test procedures are also included 5 2 Certification Procedure 5 2 1 Equipment Compatibility Careful consideration must be paid to the electrical characteristics of existing equipment or possible additions that will be interfaced to the MK VI MK VIII EGPWS in order to ensure system compatibility Section III of this manual provides system planning guidelines and defines the electrical characteristics of the EGPWS The installing agency
425. will still function for these glideslope only installations but not for those envelope modulation areas that require a localizer crosscheck 3 11 2 Glideslope Validity Glideslope Validity 28V Super Flag is required for Navigation Inputs Select 0 or 5 at pin J1 11 Glideslope Validity Low Level is required for Navigation Inputs Select 1 at pins J1 30 and J1 10 Digital 429 Glideslope interfaces do not require Glideslope Validity input 3 11 3 Localizer Validity Localizer Validity 28V Super Flag is required for Navigation Inputs Select 5 at pin J1 48 Digital 429 Localizer interfaces do not require Localizer Validity input 3 11 4 ILS Tuned Discrete Input 1 28V and 2 GND The ILS Tuned Discretes 28V and GND indicate that an Instrument Landing System frequency has been selected on the Captain s or selected ILS only one is required These discretes are used with the analog Glideslope inputs When an ILS is tuned the MK VI MK VIII EGPWS checks the Glideslope Validity discretes and monitors the Glideslope inputs Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE DWG NO 060 4314 150 REV SHEET 94 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 11 5 Analog Glideslope Interface Cat 9 ID 0 1 5 EGPWS MK VI MK VIII Jl iL Read J 65 e GS Deviation lt Up GS Deviation
426. x Range 131 072 Ft Approx LSB 1 0 Foot Data 12 to 28 17 Above Ground Level AGL Sign Bit 29 Pad Bits N A Transmit Interval msec 1000 10 Data Type 2 s Compliment Binary SDI Bits N A Set to 1 when Computed Terrain Clearance low accuracy is indicated 12 28 Computed Terrain Clearance 7 1 2 5 Latitude Selected EGPWS 310 7 1 2 6 Longitude Selected EGPWS 311 7 1 2 7 Body Angle of Attack Right 223 MKVIII EGPWS w Windshear only Data Bits 14 to 28 15 Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 100 20 Data Type 2 s Compliment Binary SDI Bits 9 10 Proprietary notice on title page applies CAGE CODE 97896 SCALE SIZE A DWG 060 4314 150 REV SHEET 308 Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 1 2 8 Body Angle of Attack Left 224 EGPWS w Windshear onl Data Bits 14 to 28 15 Sign Bit 29 Pad Bits 11 to 13 Transmit Interval mSec 100 20 Data Type 2 s Compliment Binary SDI Bits 9 10 7 1 2 9 Corrected Airspeed 242 MKVIII EGPWS w Windshear onl 7 1 2 10 Windshear Warning Threshold 331 MKVIII EGPWS w Windshear onl 7 1 2 11 Corrected Longitudinal Acceleration 332 MKVIII EGPWS w Windshear only Note Longitudinal Acceleration is corrected by Cosine of Body Angle of Attack 7 1 2 12 Raw Total Shear 362 MKVIII EGPWS w Windshear only 7 1 2 13 Corrected Normal Accele
427. x E Table 5 3 5 under the Ident No heading for Step Category 5 in Appendix E Table 5 2 Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG NO 060 4314 150 REV SHEET 68 Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 8 Category 6 Terrain Display Select Category 6 defines the Terrain Display options available TA amp D and TCF mode enabling disabling is controlled by Category 6 Peaks mode availability is controlled by Category 6 since its availability is determined by the display configuration Peaks mode enabling disabling is controlled by Category 7 Each of the options controlled by Category 6 is described below Appendix E Table 5 3 6 defines the Terrain Display Select options Display Configuration Group Tables Display Input Control Group Tables and Output 429 Bus Group Tables and identifies the first MK VI MK VIII EGPWS version in which the option was available see the Effectivity entry Appendix E Table 5 3 6 also defines the EGPWS version MK VI or MK VIII in which the option is available see the EGPWS entry Appendix E Tables 5 3 6 1 x where x is the Display Configuration group number define the display options and the electrical interface required to support each Display Configuration Appendix E Tables 5 3 6 2 x where x is the Display Input Control group number define the label set and the electrical interface required to support each Display Configuration Appendix E
428. y data to switching relay Symbol Generator 4 2 13 2 _ MEN 0 4 NI DISPLAY BUS 72 CONNECT TO PI l SI MEN MENU RE EE J1 56 Terrain Display data to switching relay Symbol Generator 4 2 13 2 Bun Sr uu Display Input Control Group 1 CHANNEL CONNECT TO WX IND Bus 1 out Fault Designation DISPLAY BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Type Basic A J2 37 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms CHANNEL CONNECT TO WX IND Bus 2 out Fault Designation DISPLAY BUS 2 429RX 3 Format ARINC 429 Low Speed Bus Basic A J2 41 Data Reference Label Sig Bits Range Signal Type Resolution Rate ms an J2 40 Range Display Word 2 2 20 271 Discrete 5 320NM Basic N A 100 1 32 GND_DISC_12 au Display Select Discrete 1 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 18 not Gnd Normal J1 31 GND DISC 13 Reference Display Select Discrete 2 Type 1 Momentary 42 7 Gnd Display Select Toggle 6 6 19 not Gnd Normal Output 429 Bus Group 0 Channel Pins Comments 429TX 1 Low Speed A J2 43 Transmits Section 7 Label sets 7 1 1 x 7 1 2 x 7 1 3 x and 7 1 4 x B J2 42 Integration Notes 1 When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels This prevents the EGPWS from reporting an external bus fault on the second channel Proprietary notice on title
429. ys are requested on label 012 Key Press Display Mode 4 The Display group is configured by the Display using response labels on its ARINC 429 data bus 5 KCPB bus types use Inop amp Warning Annunciations in same Window therefore during EGPWS Self Test the Fail lights will not remain on throughout the test Proprietary notice on title page applies CAGE CODE 97896 SCALE NONE SIZE A DWG 060 4314 150 REV SHEET 216 Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5 3 6 1 20 KC Picture Bus without presentation of Geometric Altitude Display Configuration Group 17 Display Type KC PictureBus KCPBY 2 Sweep Type Curtain Vertical or Horizontal scan 00 O Auto Pop Up 527 Peaks Mode Category 7 Options Select Group 1 5 3 7 Elevations via overlay Manual select None Display controls selection O Manual deselect 7 None Display controls selection 0 y O Auto Range Controlled by display response if selected 10 NM range willbeused Moving Marker Overlay Page Controlled by display 12 Display bus type 453 1 J1 59 7 2 453 2 B J1 57 72 Display Input Control Group 4 CHANNEL CONNECT TO KCPB IND Bus 1 out Fault Designation KCPB BUS 1 429 422RX 1 Format ARINC 429 Low Speed Bus Tvpe Basic Data Reference Sig Bits Range Signal Type Resolution Rate ms Range 6 2 35 11 0 5 1023 5NM Basic 0 5 25

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