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SMM:PRIMUS 2000 Integrated Avionics System:Falcon 900EX

1. 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 wore Function Connector Pin Connects To CTR ENG IGN 28 0 137J2A 37 SPARE 28 0 38 AIR BRAKES 1 EXTEND 28 0 39 AIR BRAKES 2 EXTEND 28 0 40 FLAPS 7 DEG SEL 28 0 41 FLAPS 20 DEG SEL 28 0 42 FLAPS 40 DEG SEL 28 0 43 EMERG SLATS EXTENDED 28 0 44 END ITEM TEST 28 0 45 CTR ENG START 28 0 46 RT BUS VOLTAGE NORM 28 0 47 RAD ALT 2 VALID 28 0 LNT TN EA aas Baan PODS P5 PO AGER annan ID 1 CHB GND OPEN 7 ID 2 CHB GND OPEN SIGNAL GND ID 3 CHB GND OPEN 9 137J2A 72 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 10 BP Function Connector Pin Connects To 137J2A 73 74 75 76 ASCB NO 1 PRI 77 DAU CHANNEL B S FIGURE 8 1 SEE 137J2A 77 ASCB NO 1 PRI H DAU CHAN
2. ARINC 429 Interfaces Figure 8 2a 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 145J1B LSS EN a al J H e pee c J gs C14 AD 42402 R1 ARINC 429 Interfaces Figure 8 2b 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont IAC 190J1C 190 1 IAC 2 L 145J1B 47 48 ARINC 429 Interfaces Figure 8 2c 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 1 190314 c190J1A IAC 21 T r 53 AD 41479 ARINC 429 Interfaces Figure 8 2d 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this documen
3. gt FP BATTERY BUS RIGHT BUS aya EXTERNAL POWER AD 41483 Power Distribution Figure 8 6a 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document l MINIMAL LOAD 2 5 MASTER SW LH AVIONICS MASTER SW Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont IRS1 BATT 170J1C 2 172J1 K 170J1C 4 80W 170J1C 7 140W AT IRS NO 1 STARTUP FAN 29W 4aH L 4 4 9 9J1 26 16W 11J1 19 21W 130J1 101 130J1 102 177W 130J1 103 115J1 59 TBD 137J2A 103 14W 137J2A 104 EST 190J1A 11 FP 190J1A 12 156W 14W 137J1A 103 EST 137J1A 104 190J1B 8 190J1B 9 69W E170J1C 4 E170J1C 7 IRS NO 3 FAN 80W 140W AT STARTUP 29W 120J1 B 120J1 v 120J1 F 1491 35 131J1 101 131J1 102 131J1 103 20J1 c 59J1 A 59J1 B 61J1 D C61J1 D 123J1 C OW 190J1D 6 190J1D 7 125W 190J1D 8 E190J1A 11 E190J1A 12 bui E190J1B 8 78 5W E190J1B 9 IRS3 BATT E170J1C 2 E172J1 K IRS2 BATT C170J1C 2 132J1 101 132J1 102 177W 132J1 103 E190J1D 6 E190J1D 7125W E190J1D 8 136J1A 103 14W 136J1A 104 EST l RH AVIONICS MASTER SW Power Distribution Figure 8 6b 22 05 21 C172J1 K C170J1C 4 80W C170J1C 7 140W AT IRS 2 STARTUP FAN 29W C9J1 26 16W 11 2 19 21W
4. 1 PANEL STROBE 1 BUTTON DATA H 1 BUTTON DATA L SPARE SPARE GND OPEN SPARE SPARE SPARE CHASSIS GND SPARE C S GND OPEN SPARE GND OPEN 1 5 VDC POWER 190J1D 95 1 5 VDC POWER RETURN S 190J1D 94 1 28 VDC POWER FIGURE 8 6 1 28 VDC POWER RETURN DC POWER GND SPARE SPARE SPARE SPARE SPARE GND OPEN SPARE SPARE SPARE C S GND OPEN 11J1 28 mn 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC cont GC 810 IO BP Function Connector Pin Connects To SPARE 11J1 29 1 SPARE GND OPEN 30 SPARE 31 1 SECONDARY TRIM DISCONNECT 32 FIGURE 8 9 C S 28V 0PEN SPARE GND OPEN SPARE GND OPEN SPARE GND OPEN SPARE GND OPEN 1 BC MODE 28V OPEN SPARE GND OPEN SPARE GND OPEN DIMMING LEVEL H FIGURE 8 7 DIMMING LEVEL L LIGHTING GND PWM ANN DRIVE PITCH WHEEL TACH H 24 yc aoe rs S T S 190J1B 11 C190J1B 11 PITCH WHEEL TACH L 190J1B 10 L GND C190J1B 10 ADI BC GND OPEN 45 1 PB ARM IN GND OPEN 46 1 PB ARM OUT GND OPEN 47 190J1A 100 SPARE SPARE SPARE 1 LAMP TEST GND OPEN FIGURE 8 7 SPARE GND OPEN 12 L SEL BUTTON GND OPEN 53 12 R SEL BUTTON GND OPEN 54 2 DISABLE GND OPEN 55 2 RESET
5. FIGURE FIGURE FIGURE FIGURE FIGURE 2 2 2 2 2 2 2 2 2 2 2 2 Ae AR Ae Ae Ae nn coco nn nn 2 AA AA AA AA aa 2 2 RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST 69 RESERVED FOR TEST 137J1B 70 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 10 BP Function Connector Pin Connects To 137J1B 71 72 2 RADIO ALTIMETER 2 RADIO ALTIMETER FIGURE 8 13 NORMAL ACCELERATION NORMAL ACCELERATION ASCB NO 2 BU DAU CHANNEL A S T S FIGURE 8 1 5 96 SEE 137J1B 94 97 RESERVED 98 RESERVED 99 RESERVED 100 RESERVED 101 102 103 RS 232 DATA CH A XMTR 104 24 S RS 232 DATA CH A RCVR 105 24 S FIGURE 8 3 RS 232 CH A COMMON 137J1B 106 24 EE ND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information c
6. 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 4 1 3 5 SYSTEM MAINTENANCE Honeywell MANTEN Table 3 1 Interconnect Information cont Connector Wire Size FALCON 900EX Table 4 1 contains a list of system connectors and the maximum allowable gauge wire that each can accept Wiring that comes into these connectors that has a larger gauge than the connecter pin will allow must be spliced down to the proper gauge Table 4 1 Connector Wire Gauge Limitations Unit Component 9 AZ 840 11 GC 810 SM 200 SM 725 RT 300 WU 870 WC 880 DC 840 CD 810 DL 900 SM 810 DU 870 RC 820 RC 841 Connector MS27473E20B 35S J1 MS27473E20B 35SB J2 MS27473E20B 35SD J3 MS27473E12A 22S MS3126F14 19S MS3122E14 19S MS3126F16 26S MS3126F22 55S J1 MS27473E14B 18S J3 MS27473E14A 18SB J1 MS27473E20B 35S J2 MS27473E14 35S MS3126F22 55SX MS3126F16 265 MS3106A 16S 1S DPXBMA A106 33P 0415 MS27473E16A 35S MS27473E16A 35SA 22 05 21 Wire Gauge 79 22 AWG 79 79 22 22 AWG 22 AWG 22 AWG 19 20 AWG 19 20 AWG 26 20 AWG 18 18 20 AWG 20 AWG 79 37 22 AWG 22 AWG 55 20 AWG 55 20 AWG 26 20 AWG 7 16 AWG 106 22 AWG 55 22 AWG 55 22 AWG Page 3 13 Sep 1 1996 Use or disclosure of information on this page is s
7. YS SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont MICRO AIR DATA COMPUTER MADC NO 1 cont AZ 840 Function Connector Pin Connects To ASCB NO 1 BACKUP H 9J1 59 ASCB NO 1 BACKUP L 62 ARINC 429 BUS 1 FIGURE 8 1 60 H ARINC 429 BUS 1 L 61 S S FIGURE 8 2 62 ARINC 429 BUS 2 H 63 ARINC 429 BUS 2 1 64 ASCB NO 2 PRI H 65 ASCB NO 2 PRI L 77 ARINC 429 BUS H 66 ARINC 429 BUS L 67 3 H 3 L ARINC 429 BUS 4 H 68 ARINC 429 BUS 4 L 69 FIGURE 8 2 FIGURE 8 1 FIGURE 8 2 nn nn 2 AA AA AA 2 FIGURE 8 2 FUNCTIONAL TEST GND OPEN 70 FIGURE 8 8 BARO STD SYNC GND OPEN 71 130J1 46 SSEC DISABLE 72 FIGURE 8 8 SPARE 73 BARO CORRECTION 74 130J1 21 BARO CORRECTION 75 130J1 25 SPARE 76 77 SEE 901 65 SPARE 78 SPARE 9J1 79 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC GC 810 Function Connector Pin Connects To 1 ANN DATA H 1141 1 1 ANN DATA L 2 1 PANEL CLOCK 1 PANEL CLOCK L 190J1D 99 190J1D 98 190J1D 97 190J1D 96 190J1D 51 190J1D 50 190J1D 63 190J1D 62 T MN no no Po no fH HSH FH FH 1 PANEL STROBE H L
8. 1 POSITION AIRCRAFT RADAR SYSTEM TO FACE AWAY FROM BUILDINGS LARGE METAL STRUCTURES OR OTHER AIRCRAFT IN CLOSE PROXIMITY BEFORE YOU TURN IT ON THEY ARE LIKELY TO RETURN LARGE AMOUNTS OF REFLECTED ENERGY AND CAUSE DAMAGE TO THE SYSTEM DO NOT OPERATE RADAR WITHIN 50 FEET OF OTHER AIRCRAFT OR OBJECTS OR CLOSER THAN 100 FEET TO REFUELING OPERATIONS NEVER LOOK DIRECTLY INTO THE ANTENNA WHILE IT IS OPERATING FOR PROLONGED PERIODS OF TIME AT A CLOSE RANGE SERIOUS EYE TISSUE DAMAGE CAN RESULT DUE TO THE HEATING EFFECT OF RADAR ENERGY THE MAXIMUM PERMISSIBLE EXPOSURE LEVEL MPEL BOUNDARY IS A RADIUS OF 12 FT 366 CM REFERENCE SECTION 2 CHAPTER 5 FOR DETAILS a Before applying power to the radar set SCAN and XMTR toggle switches on the WU 870 housing to OFF toward antenna b Level the pitch and roll axes of the aircraft relative to the earth s surface c Verify that the mounting surface of the WU 870 is aligned to the pitch and roll reference axes of the aircraft within 1 4 degree d Apply aircraft power as necessary 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX On the WC 880 Weather Radar Controller make the following selections RADAR SBY e TILT 0 e GAIN Push knob in for preset gain Verify in the SBY mode that the flat plate antenna is at 0 within 1 2
9. H A 429 RCVR 4 1 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED IRS DATA OUT 3 H ARINC 429 XMTR L RESERVED K14 RESERVED C170J1B K15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Function Connector Pi Connects To 115 VAC INPUT C170J1C 1 24 VDC BATT INPUT 2 FIGURE 8 6 RESERVED 3 28 VDC ESSENTIAL 4 FIGURE 8 6 115 VAC RETURN 5 28 VDC MSU POWER OUTPUT 28 VDC PRIMARY POWER FIGURE 8 6 28 VDC BATTERY POWER RTN DC POWER GND ANNUNCIATOR POWER OUT C172J1 L ANNUNCIATOR POWER IN FIGURE 8 7 CHASSIS GND RESERVED 12 RESERVED C170J1C 13 TRAY FAN POWER RED C170J1C 7 TRAY FAN POWER GND BLK 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP 1 SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont TRS MODE SELECTION UNIT NO 2 MSU Function Connector Pin Connects To CHASSIS GND 172 1 SPARE B SPARE SPARE SPARE SPARE SPARE SPARE SPARE ON BATT ANNUN PWR INPUT FIGURE 8 6 ANNUN PWR C170J1C 9 28 VDC IRU BLOWER M IRU BLOWER CONTROL 28V 0PEN FAULT ANNUN GND OPEN C170J1B D2 SPARE
10. 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AUTOTHROTTLE SERVO NO 1 SM 810 Function Connector Pi Connects To SERVO TACH 128J1 A E190J1D 59 CCW ROTATION L D E190J1D 58 SERVO DRIVE E190J1C 1 CCW ROTATION L E190J1C 2 GND L GND SEE 128J1 A SERVO CLUTCH S E190J1C 12 LGND C128J1 E SERVO CLUTCH DC POWER GND CHASSIS GND 128J1 G 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AUTOTHROTTLE SERVO NO 3 SM 810 Function Connector Pi Connects To SERVO TACH E128J1 A E190J1D 55 CCW ROTATION D E190J1D 54 SERVO DRIVE E190J1C 26 CCW ROTATION E190J1C 13 GND L_GND SEE E128J1 A SERVO CLUTCH Sess E190J1C 10 ND SERVO CLUTCH DC POWER GND CHASSIS GND E128J1 G 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 1 DU 870 Function Connector Pin Connects To 130J1 1 135J1 1 13 24 135J1 3 14 135J1 2 H BRIGHTNESS POT L W
11. A Removal and Reinstallation Procedures 1 Remove mounting tray Remove unit fan and filter as instructed in paragraphs 15 16 and 17 Remove and set aside the four nuts four washers and four screws that attach the ARINC 600 connector to the rear of the mounting tray Detach the ARINC 600 connector Remove and set aside the four screws and four washers that attach the mounting tray to the airframe 2 Reinstall mounting tray NOTE The accuracy of attitude angle indication is directly dependent upon the accuracy with which the IRU is aligned with the aircraft axes The mounting tray must be installed with a relative alignment accuracy of 0 2 degree in the pitch roll and yaw axes Using the mounting hardware previously removed and set aside attach the mounting tray to the airframe Screws should be tight enough to prevent movement of the tray Using the connector hardware previously removed and set aside install the ARINC 600 connector making sure to leave a maintenance loop in the harness of sufficient length so as not to apply any pressure on the mounting tray Level the tray in accordance with one of the two methods specified in paragraphs 18 B 1 and 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Adjustment Procedures Align the mounting tray with the three axes of t
12. 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA LOADER DL 900 Function Connector Pin Connects To RESERVED PWRVAL 123J1 A 28 VDC POWER RETURN B DC POWER GND 28 VDC POWER C FIGURE 8 6 LOADER CONNECTED RIGHT D C190J1D 4 GND OPEN LOADER CONNECTED LEFT E 190J1D 4 GND OPEN LOADER CONNECTED AUX F E190J1D 4 GND OPEN DATA IN L G 190J1A 46 RS 422 RCVR C190J1A 46 E190J1A 46 H 190J1A 45 G C190J1A 45 E190J1A 45 CLK IN L 190J1A 98 RS 422 RCVR C190J1A 98 E190J1A 98 H 190J1A 97 G C190J1A 97 E190J1A 97 RESERVED SELFTEST RESERVED BAUDSEL RESERVED TESTDIS RESERVED VPP SIGNAL GROUND SIGNAL GND DATA OUT 190J1A 64 RS 422 XMTR 190 1 64 E190J1A 64 190J1A 63 C190J1A 63 E190J1A 63 SPARE U RS 232 COMMON V RS 232 XMTR Z RS 232 RCVR 123J1 a FIGURE 8 3 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA LOADER cont 0 Function Connector Pin Connects To RS 232 DATA SET RDY 123J1 W RS 232 CLR TO SEND X RS 232 REQ TO SEND SEE 123J1 V SEE 123J1 V CHASSIS GND b SPARE 123J1 c
13. E172J1 C170J1A LOGIC GND IRU ORIENT 1 IRU ORIENT 2 SDI 2 575 429 ADC SDI 1 L MSU 2 LOGIC GND C172J1 DIRECTION HANDLES POINT PROGRAM PIN FWD LEFT RIGHT J1B A2 J1B A1 JUMPER TO OPEN JUMPER TO J1B A1 J1B A3 OPEN JUMPER TO J1B A1 JUMPER TO J1B A1 AD 41482 IRS Strapping Figure 8 4 Page 3 218 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont 9J1 12 C9J1 12 1171 58 61 1 1491 28 C149J1 28 190J1D 103 C190J1D 103 E190J1D 103 Y 136J2A 13 137J2A 13 WEIGHT ON LEFT MAIN GEAR Y 136J2A 14 137J2A 14 WEIGHT ON NOSE GEAR 1 y i 136J2A 15 137J2A 15 WEIGHT ON RIGHT MAIN GEAR AD 41496 Weight on Wheels Switch Diagram Figure 8 5 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 0 4 gt BUS A1 1 5 gt gt BUS A2 e1 5 V 9 BUS Io 9 BUS 4 5 V BUS A5 e gt BUS LEFT BUS MANUAL BUS TIE OFF IN FLIGHT
14. H L W f 2 WX DIMMING L 3 15 RESERVED 4 RESERVED 5 RESERVED RESERVED SPARE RESERVED RESERVED RESERVED RESERVED 13 SEE 130J1 1 14 SEE 130J1 1 15 SEE 130J1 2 RESERVED 16 RESERVED 17 RESERVED BUS 3 H 19 BUS 3 NO TERM 1 20 FIGURE 8 14 GND L GND BARO KNOB B0 21 DU PWR DN GND OPEN 22 135J1 8 0 5 VDC EDGE H 23 FIGURE 8 7 LIGHTING L 24 LIGHTING GND BARO KNOB B1 25 REMOTE LT SENSOR H 26 REMOTE LT SENSOR L 130J1 27 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MAINTE FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 1 cont DU 870 Function Connector Pin Connects To DLS H 130J1 28 24 s 131J1 29 DLS L 41 24 S 131 1 42 GNo ALS H 29 24 s ALS L 24 5 GND RESERVED RESERVED HDLC OUT RESERVED HDLC OUT BUS 3 TERM RESERVED BUS 2 FED BUS 2 NO TERM 1 DU VALID GND OPEN BUS 1 han BUS 1 NO TERM 1 REMOTE LT SENSOR GND SEE 130J1 28 SEE 130J1 29 RESERVED RESERVED BUS 4 TERM DU 1 PB5 STD GND OPEN DU 1 PB4 IN HPA 115J2 12 GND OPEN C115J2 12 RESERVED BUS 2 TERM 49 DU 1 PB3 METRIC 50 115J2 11 GND OPEN C115J2 11 DU 1 PB2 FORMAT 51 115J2 10 GND OPEN C115J2 10 BUS 1 TERM 52 5
15. 0 5 VDC PANEL LIGHTING H S 0 5 VDC PANEL LIGHTING L T LOGIC GND U TEST GND V TEST SW GND OPEN W NAV RDY ANNUN GND OPEN X NO AIR ANNUN GND OPEN Y BATT FAIL ANNUN GND OPEN Z ALIGN ANNUN GND OPEN a SPARE b SPARE SPARE d MODE SELECT 1 e C170J1B F1 MODE SELECT 2 f C170J1B F2 ON BATT ANNUN g C170J1B J15 GND OPEN ANNUN TST GND OPEN h FIGURE 8 7 SPARE C172J1 j FIGURE 8 7 LIGHTING GND FIGURE 8 4 SIGNAL GND C170J1B A10 C170J1B E3 C170J1B E1 C170J1B A15 C170J1B F3 RO 5 Ro Ro Po annn 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 0 Function Connector Pin Connects To SIGNAL GROUND C190J1A 1 22 SIGNAL GND 28V ELEV TRIM CLUTCH OUT 2 TAC IDENT 2 GND OPEN 3 FGC RESERVED 4 ASCB NO 2 BU H ASCB NO 2 BU 1 FIGURE 8 1 BC RS 232 DATA RCVR BC RS 232 DATA XMTR FIGURE 8 3 BC DL RS 232 COMMON 28 VDC AP SERVO PWR RIN DC POWER GND 28 VDC AP SERVO PWR RTN DC POWER GND BC RESERVED 28 VDC AP SERVO POWER 28 VDC AP SERVO POWER FIGURE 8 6 SPARE H IOP RS 422 TX L DU 4 WRAPAROUND L C131J1 79 A 429 RCVR 12 190J1A 15 E190J1A 15 H C131J1 66 190J1A 16 E190J1A 16 TAG SYNC IN 1 17 190J
16. 104 TRIM RATE CMD OUT L 105 N CROSS YD PWR SENSE IN 190J1A 106 24 C190J1C 4 28 V OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 Function SPARE FMS DISC IN GND OPEN YD POWER RETURN YD POWER RETURN 28 VDC AIRCRAFT RAM BATTERY L H Connector Pin 190J1B 1 FWC RESET GND OPEN FGC RESERVED 28V YD SERVO POWER 28V YD SERVO POWER PITCH WHEEL 1 PITCH WHEEL 1 SPARE FMS DISC GND OPEN ASCB NO 2 PRI ASCB NO 2 PRI RSB RSB RSB RSB RSB RSB RSB RSB RSB RSB H L RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RSB RESERVED RSB RESERVED WX 2 RANGE UP OUT GND OPEN WX 2 RANGE DN OUT GND OPEN WX 1 RANGE UP OUT GND OPEN L H zi 3 4 5 6 f 8 59 10 24 S T S 11 24 12 13 GND SEE 190J1B 13 L_GND 28 24 190J1B 29 24 22 05 21 Connects To DC POWER GND FIGURE 8 6 1101 44 C190J1B 10 1101 43 C190J1B 11 FIGURE 8 1 C61J1 L C190J1B 27 E190J1B 27 C61J1 N C190J1B 28 E190J1B 28 61J1 L C190J1B 29 E190J1B 29 Page 3 117 Sep 1 1996 Use or disclosure of informa
17. 2 S38 24 yo S T S 115 1 7 IOP RS 422 RX E190J1C 38 L 39 C115J1 8 L GND 190J1C 39 FGC RESERVED 40 SPARE FGC DISC IN 190J1C 41 28V 0PEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pin Connects To FGC RESERVED 190J1C 42 FGC RESERVED 43 CROSS AP PWR SENSE 44 C190J1A 93 OUT 28 V OPEN FGC RESERVED 45 FGC RESERVED 46 FGC RESERVED 47 FMS CDU DTR OUT 48 S 120J1 V FMS RS 422 TX H 49 S 120J1 U FGC RESERVED 50 FMS CDU DATA OUT L 51 120J1 T FMS RS 422 TX H 52 S 120J1 S SPARE CARD RESERVED 53 SPARE CARD RESERVED 54 CROSS CHANNEL SYNC OUT 55 C190J1A 92 GND OPEN SPARE FGC DISC IN 56 28V 0PEN FGC RESERVED 57 FMS CDU CTS IN K 58 S 120J1 R FMS RS 422 RX H 59 S T S 120J1 P L_GND SPARE FGC ANALOG IN H 60 SPARE FGC ANALOG IN L 61 FGC RESERVED 62 FMS CDU CLOCK OUT 63 120J1 X FMS RS 422 TX 64 TCAS 65 A 429 RCVR 6 66 S FIGURE 8 2 SPARE CARD RESERVED 67 SPARE FMS DISC OUT 190J1C 68 GND OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAIN
18. 2 2 2 2 2 2 BE AR Ae Ae Ae nn coco nn nn 2 AA AA AA AA AA aa 2 2 RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST RESERVED FOR TEST 69 RESERVED FOR TEST 136J1B 70 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 Function Connector Pin Connects To 136J1B 71 72 1 RADIO ALTIMETER 1 RADIO ALTIMETER FIGURE 8 13 GND L GND SPARE DC ANALOG SPARE DC ANALOG ASCB NO 1 BU DAU CHANNEL A FIGURE 8 1 5 96 SEE 136J1B 94 97 RESERVED 98 RESERVED 99 RESERVED 100 RESERVED 101 102 103 RS 232 DATA CH A XMTR 104 24 RS 232 DATA CH RCVR 105 24 FIGURE 8 3 RS 232 CH A COMMON 136J1B 106 24 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 wore Function Connector Pi
19. 2 L 84 L RESERVED SBY ENG ENABLE 85 GND OPEN SPARE DIO DISC IN 86 GND OPEN SPARE DIO DISC IN 87 GND OPEN RESERVED FWC MEM ERASE 88 GND OPEN 28V AP CLUTCH IN C190J1D 89 S 12J1 G 28V 0PEN 13J1 G 190J1C 12 C190J1C 12 190J1D 89 E190J1D 89 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To I RESERVED FWC C190J1D 90 DOWNLOAD INIT GND OPEN 1 28V YD BRAKE IN 91 14J1 E 28V 0PEN G 190J1C 10 C190J1C 10 190J1D 91 E190J1D 91 SPARE DIO DISC IN GND OPEN COPILOT STICKSHAKER FIGURE 8 12 28V 0PEN GC PANEL POWER RETURN 1102 18 5V GC PANEL POWER 1142 17 GC PANEL CLOCK 1142 4 GC PANEL CLOCK S T S 11J2 3 GC PANEL ANNUN DATA L 11J2 2 GC PANEL ANNUN DATA H S T S 11J2 1 TRIM ARM UP OUT FIGURE 28V 0PEN FMS RESET GND OPEN SPARE DIO DISC IN GND OPEN WEIGHT ON WHEELS FIGURE GND OPEN ASCB NO 2 PRI ASCB NO 2 PRI L 5 FIGURE TRIM ARM DN OUT FIGURE 28V 0PEN C190J1D 106 SEE C190J1D 104 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL
20. A conductive coating should be used for corrosion prevention A suitable commercial product is Alodine 1201 which can be brush applied b Place new gasket Honeywell Part No 4010193 6 on antenna c Connect TNC cable connector d Mount antenna and apply applicable sealant such as No DC 3145 RTV e Install the four No 10 corrosion resistant steel pan head screws that were removed and previously set aside 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX AFT AD 43787 0 Figure 4 1 AT 300 Radio Altimeter Antenna Orientation Adjustment Procedures Not Applicable Repair Procedures Not Applicable 22 05 21 Sen 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell awe FALCON 900EX 4 Procedure for the AZ 840 Micro Air Data Computer MADC A Removal and Reinstallation Procedures 1 Remove MADC a Disconnect pitot and static lines Cap or cover hose end connectors to keep debris out of the system b Disconnect cable connector c Using a 3 16 inch Allen wrench loosen jackscrew until hold down hook releases MADC d Slide MADC out of tray 2 Reinstall a Slide into mounting tray b Make sure that the rear boss engages the mounting tray slot c Mak
21. ANTENNA L490 251 sss 0 GPS ANTENNA ANTENNA 149J2 2 L GPS ANTENNA PIC WIRE AND CABLE PART NO T556124 FOR 13 FT LENGTH FOR SMALLER SECTION USE PART NO SF 5224 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 LASEREF III Function Connector Pin Connects To IDENT RESISTOR R1 170J1A Al RESERVED A2 RESERVED RESERVED RESERVED RESERVED 6 SDI 4 GND OPEN FIGURE 8 4 RESERVED 8 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED IDENT RESISTOR R2 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 170J1A B15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Function Connector Pin Connects To IDENT RESISTOR R3 170 1 1 IDENT RESISTOR COM C2 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED ASCB NO 1 PRI H ASCB NO 1 PRI L FIGURE 8 1 GND L GND RESERVED RESERVED RESERVED RE
22. C170J1B F15 24 S T GND L GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Function Connector Pin Connects To RESERVED C170J1B G1 RESERVED G2 RESERVED RESERVED RESERVED RESERVED IRS DATA OUT 1 ARINC 429 XMTR RESERVED RESERVED RESERVED RESERVED RESERVED IRS DATA OUT 5 ARINC 429 XMTR RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED H13 IRS DATA OUT 6 H14 ARINC 429 XMTR L 170218 H15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III 10 BP Function Connector Pin Connects To RESERVED C170J1B J1 RESERVED J2 RESERVED J3 RESERVED J4 RESERVED J5 DADC 575 429 SEL J6 FIGURE 8 4 RESERVED J7 RESERVED J8 501 1 GND OPEN J9 24 FIGURE 8 4 SEC DADC DATA H J10 A 429 RCVR 5 L J11 RESERVED J12 RESERVED J13 RESERVED J14 ON BATTERY ANNUN J15 C172J1 g RESERVED K1 RESERVED K2 RESERVED K3 PRI DADC DATA K4
23. GND OPEN 11J1 56 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC cont GC 810 Function Connector Pin Connects To 1 ANN VALID 28V OPEN 1101 57 24 190J1D 14 Uic Pur TCS PB C S GND OPEN 60 24 FIGURE 8 11 SPARE GND OPEN SPARE SPARE GND OPEN SPARE C S 28V OPEN 11 L SEL BUTTON GND OPEN 65 11 R SEL BUTTON GND OPEN 66 111 DISABLE GND OPEN 67 1 RESET GND OPEN 68 SPARE 69 SPARE GND OPEN 70 1 AP DISCONNECT GND OPEN E FIGURE 8 11 SPARE C S GND OPEN 72 SPARE 28V OPEN 73 SPARE C S GND OPEN 74 AP DISENG ANN GND OPEN 75 SPARE C S GND OPEN 76 SPARE GND OPEN 77 0 5 VDC EDGE H 78 22 FIGURE 8 7 LIGHTING L 11J1 79 22 LIGHTING GND mmm wee 0 0 0 0 0 an wwe 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC cont GC 810 Function Connector Pin Connects To 2 ANN DATA H 24 one S C190J1D 99 2 ANN DATA L 2 24 9 02 S C190J1D 98 GND 12 PANEL
24. H 55 l l 14J1 N G C190J1D 55 YD LVDT FEEDBACK SPARE FGC RVDT 56 ANALOG IN 57 58 12J1 N AILERON TACH C190J1D 58 59 12J1 L C190J1D 59 L 60 13J1 N ELEVATOR TACH C190J1D 60 H 61 13J1 L G C190J1D 61 GC PANEL L 62 1101 8 BUTTON DATA 63 S T 11 1 7 AWP ENABLE 28V 0PEN 64 SPARE FGC DISC IN 65 28V 0PEN BC ID 1 GND OPEN 190J1D 66 SIGNAL GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 Function Connector Pin Connects To SPARE FMS DISC OUT 190J1D 67 GND OPEN FMS VTA HORN GND OPEN 68 FIGURE 8 15 SWITCHED L 69 14J1 V LVDT RVDT l C190J1D 69 EXCITATION 70 14 1 0 L GND C190J1D 70 RESERVED HDLC RX 1 RESERVED HDLC RX 1 L 71 72 FGC RESERVED 73 FGC RESERVED 74 CROSS SERVOS OFF 28V 0PEN 75 C190J1A 90 CROSS SERVOS PWR OFF 76 C190J1A 91 28V 0PEN AIL RVDT SURFACE POS 77 AIL RVDT SURFACE POS 78 BC ID 3 GND OPEN 79 IOP RS 232 COMMON 80 IOP RS 232 DATA XMTR 81 FIGURE 8 3 IOP RS 232 DATA RCVR 82 RESERVED HDLC RX 2 H 83 RESERVED HDLC RX 2 L 84 L RESERVED SBY ENG ENABLE 85 GND OPEN SPARE DIO DISC IN 86 GND OPEN SPARE DIO DISC IN 87 GND O
25. IAC DU WX Interfaces Figure 8 14 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AP OFF HORN 190J1B fiac 34 44 a 44 CHECK PFD ANNUNCIATOR L 190J1D IN WARNING PANEL fiac 3 E190J1B 34 B ALTITUDE ALERT HORN E190J1D E 190J1B 2 C190J 34 44 44 C190J1D VERTICAL TRACK ALERT HORN AD 41504 Alt Alert AP Off VTA Horns and Check PFD Annunciators Figure 8 15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont IAC 1 EVENT MARKER IAC 3 EVENT MARKER IAC 2 EVENT MARKER DAU 1 AD 41505 Pilot Event Marker Figure 8 16 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Blank Page 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Inte
26. Removal and Reinstallation Procedures 1 Remove fan a Remove the fan filter as previously instructed in paragraph 16 A 1 b There are two wires one red one black coming out of the fan housing see Figure 4 3 Disconnect these wires at their source c Turn the rim clamps until the flat edge of each clamp is facing toward the fan d Separate the fan from the fan mounting plate 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX 2 Reinstall fan a Place the fan in position on mounting tray making sure that the AIRFLOW arrow on the fan points down b Secure the fan to the base of the tray with three rim clamps Make sure that the flat edge of the rim clamp faces away from the fan c Connect the red wire to the 28 V dc source d Connect the black wire to the ground source Adjustment Procedures Not Applicable Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 18 Procedure for the IRU Mounting Tray CAUTION THE PHYSICAL MECHANICAL INSTALLATION OF THE MOUNTING TRAY FOR THE IRU HAS A VERY LARGE EFFECT ON THE ACCURACY OF ATTITUDE AND HEADING DATA DO NOT REMOVE THE TRAY UNLESS IT HAS BEEN DAMAGED OR DEFORMED
27. Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 0 BP Function Connector Pin Connects To V L 1 C19021C 99 A 429 RCVR 3 100 FIGURE 8 2 DME 1 101 429 RCVR 2 102 FIGURE 8 2 105 FIGURE 8 2 ADF 1 A 429 RCVR 1 SPARE CARD RESERVED 105 SIGNAL GROUND C190J1C 106 SIGNAL GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pi Connects To I RESERVED LX ON C190J1D 1 OPEN GND 1 TAC 3 OVERHEAT GND OPEN 2 190J1D 2 E190J1D 2 E190J1B 67 POWER SUPPLY RESERVED 3 FMS DATA LDR CONNECTED 4 123J1 D GND OPEN POWER SUPPLY RESERVED 28V IAC POWER 28V IAC POWER FIGURE 8 6 28V IAC POWER FGC RESERVED TAC POWER RETURN TAC POWER RETURN DC POWER GND TAC POWER RETURN FGC RESERVED GC PANEL ANN VALID 1102 57 28V 0PEN SPARE FGC DISC IN GND OPEN YD ACTUATOR EXTENDED 190J1D 16 YD ACTUATOR RETRACTED 14J1 D 190J1D 17 FGC RESERVED FGC RESERVED PITCH WHEEL 2 PITCH WHEEL 2 NON SWITCHED LVDT RVDT EXCITATION TRIM POSITION H 4 TRIM POSITION L C190J1D 25 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restri
28. 1 Interconnect Information cont AUTOTHROTTLE SERVO NO 2 SM 810 Function Connector Pi Connects To SERVO TACH ren C128J1 A E190J1D 61 CCW ROTATION L D E190J1D 60 SERVO DRIVE E190J1C 3 CCW ROTATION L E190J1C 5 GND L GND SEE C128J1 A SERVO CLUTCH S E190J1C 12 LGND 128J1 E SERVO CLUTCH DC POWER GND CHASSIS GND C128J1 G 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 5 DU 870 Function Connector Pin Connects To C13001 1 C135J1 1 13 24 135 1 3 14 135 1 2 BRIGHTNESS POT L W H L W f 2 WX DIMMING L 3 15 RESERVED 4 RESERVED 5 RESERVED RESERVED SPARE RESERVED RESERVED RESERVED RESERVED 13 SEE C130J1 1 14 SEE 130401 1 15 SEE C130J1 2 RESERVED 16 RESERVED 17 RESERVED BUS 3 H 19 BUS 3 NO TERM 1 20 FIGURE 8 14 GND Lend BARO KNOB BO Ren C9J1 74 DU PWR DN GND OPEN 22 C135J1 8 0 5 VDC EDGE H 23 FIGURE 8 7 LIGHTING L 24 LIGHTING GND BARO KNOB B1 25 C9J1 75 REMOTE LT SENSOR H 26 REMOTE LT SENSOR L C130J1 27 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Tab
29. 1 Interconnect Information cont REVERSIONARY CONTROLLER NO 3 cont RC 841 10 BP Function Connector Pin Connects To SPARE E135J1 32 SPARE 33 SPARE SPARE SPARE SPARE NORM GND OPEN C135J1 44 NORM GND OPEN 135J1 44 REV GND OPEN C190J1D 53 REV GND OPEN E190J1D 53 REV GND OPEN 190J1D 53 REV GND OPEN C135J1 46 REV GND OPEN 135J1 46 REV GND OPEN 135J1 32 NORM GND OPEN 135J1 24 TEST PB GND OPEN E190J1B 51 115J2 17 C115J2 17 SIGNAL GROUND SIGNAL GND DAU 1 REV PB GND OPEN 51 115J1 58 C115J1 58 DAU 2 REV PB GND OPEN 52 115J1 60 C115J1 60 5 VDC LIGHTING 53 FIGURE 8 7 LIGHTING COMMON 54 LIGHTING GND 28 VDC LIGHTING E135J1 55 mI ESRD O GO OG O 2 aaa 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 DA 800 10 BP Function Connector Pin Connects To RESERVED 136J1A 1 RESERVED 2 RESERVED 23 RESERVED 4 RESERVED 5 RESERVED 6 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 35 RE
30. 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Function Connector Pin Connects To LOGIC GROUND TRU ORIENT 1 TRU ORIENT 2 RESERVED RESERVED RESERVED SDI 2 GND OPEN FMS PRI GEN BUS H A 429 RCVR 1 L REMOTE TEST GND OPEN RESERVED RESERVED ISDU NDU NO 3 A 429 RCVR L N BATTERY FAIL ANNU GND OPEN RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 170J1B Al FIGURE 8 4 A2 FIGURE 8 4 A3 FIGURE 8 4 A4 A5 A6 A7 FIGURE 8 4 A8 A9 A10 24 172J1 W All Al2 A13 A14 A15 24 170J1B B15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Function Connector Pin Connects To RESERVED 170J1B C1 RESERVED C2 RESERVED C3 RESERVED C4 FMS SEC GEN BUS H A 429 RCVR 2 L C6 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED FAULT ANNUNCIATOR GND OP
31. 103 tt ie E FIGURE 8 2 tt ADF 1 429 RCVR 1 FIGURE 8 2 SPARE CARD RESERVED 105 SIGNAL GROUND 190J1C 106 SIGNAL GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pi Connects To I RESERVED LX ON 190J1D 1 OPEN GND 1 TAC 3 OVERHEAT GND OPEN 2 C190J1D 2 E190J1D 2 E190J1B 67 POWER SUPPLY RESERVED 3 FMS DATA LDR CONNECTED 4 123J1 E GND OPEN POWER SUPPLY RESERVED 28V IAC POWER 28V IAC POWER FIGURE 8 6 28V IAC POWER FGC RESERVED TAC POWER RETURN TAC POWER RETURN DC POWER GND TAC POWER RETURN FGC RESERVED GC PANEL ANN VALID 1101 57 28V 0PEN SPARE FGC DISC IN GND OPEN YD ACTUATOR EXTENDED C190J1D 16 YD ACTUATOR RETRACTED 14J1 D C190J1D 17 FGC RESERVED FGC RESERVED PITCH WHEEL 2 PITCH WHEEL 2 NON SWITCHED LVDT RVDT EXCITATION TRIM POSITION H 4 TRIM POSITION L 190J1D 25 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Conne
32. 2 0 3 31 3 32 Record of Revisions 3 33 RR 1 3 34 RR 2 3 35 3 36 List of Effective Pages 3 37 LEP 1 3 38 LEP 2 3 39 LEP 3 3 40 LEP 4 3 41 3 42 Section 3 3 43 System Interconnects 3 44 3 1 3 45 3 46 3 47 3 48 3 49 3 50 3 51 3 52 3 53 3 54 3 55 3 56 3 57 3 58 3 59 3 60 3 61 3 62 3 63 3 64 3 65 3 66 3 67 3 68 3 69 3 70 3 71 3 72 CO CO CO CO CO CO CO CO CO OOOOoOocococcocococococoocoococoococoocoococooococoo 2 3 4 5 6 7 8 9 2 3 3 4 i ed 41 1 4 2 2 2 2 2 2 2 2 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX SUBHEADING AND PAGE REVISION SUBHEADING AND PAGE REVISION Section 3 cont 3 119 0 System Interconnects 3 120 0 3 73 0 3 121 0 3 74 0 3 122 0 3 75 0 3 123 0 3 76 0 3 124 0 3 77 0 3 125 0 3 78 0 3 126 0 3 79 0 3 127 0 3 80 0 3 128 0 3 81 0 3 129 0 3 82 0 3 130 0 3 83 0 3 131 0 3 84 0 3 132 0 3 85 0 3 133 0 3 86 0 3 134 0 3 87 0 3 135 0 3 88 0 3 136 0 3 89 0 3 137 0 3 90 0 3 138 0 3 91 0 3 139 0 3 92 0 3 140 0 3 93 0 3 14
33. 2 1 LRN 3 1 ASCB Sensor 1 Default Type 1 Discrete ASCB Sensor 1 Default Type Config 34 AHRS or No Sensor 0 IRS Installed 1 ASCB Sensor 2 Default Type 1 Discrete ASCB Sensor 2 Default Type Config 35 AHRS or No Sensor 0 IRS Installed 1 ASCB Sensor 3 Default Type 1 Discrete ASCB Sensor 3 Default Type Config 36 AHRS or No Sensor 0 IRS Installed 1 ASCB Sensor 4 Default Type 1 Discrete ASCB Sensor 4 Default Type Config 37 AHRS or No Sensor 0 IRS Installed 1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont Radio Interface Type 3 Discretes Radio Interface Type Config 40 Config 39 Config 38 Honeywell RSB Radios 0 1 0 A429 PROLINE 0 0 1 1 of ATC s Installed 2 Discretes of ATC s Installed Config 42 Config 41 No ATC 0 Single ATC 0 Dual ATC 1 Triplex ATC 1 TCAS Installed 1 Discrete TCAS Installed Config 43 TCAS Not Installed 0 TCAS Installed 1 1 of ADF s Installed 2 Discretes of ADF s Installed Config 45 Config 44 No ADF 0 Single ADF 0 Dual ADF 1 Triplex ADF 1 1 of DME s Installed 2 Discretes of DME s Installed Config 47 Config 46 No DME 0 Single DME 0 Dual DME 1 Triplex DME 1 1 of MLS s Installed 2 Discretes dt of MLS s Installed Config
34. 211 0 4 8 0 3 212 0 4 9 0 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX SUBHEADING AND PAGE REVISION SUBHEADING AND PAGE REVISION Section 4 cont Section 5 Maintenance Practices Shipping Handling and Storage 4 10 4 11 4 12 4 13 4 14 4 15 4 16 4 17 4 18 4 19 4 20 4 21 4 22 4 23 4 24 4 25 4 26 4 27 4 28 4 29 4 30 4 31 4 32 4 33 4 34 4 35 4 36 4 37 4 38 4 39 4 40 4 41 4 42 4 43 4 44 4 45 4 46 4 47 4 48 4 49 4 50 5 2 Table of Contents Section 6 TC6 1 0 TC6 2 0 Section 6 Honeywell Support 6 1 1 OOOOoOOoOocococoOoOoOoOooocooocoocoococoocooococooocooocoocooocooco 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX SECTION 3 SYSTEM INTERCONNECTS This section provides interconnect information as an aide in troubleshooting the PRIMUSG 2000 Integrated Avionics System The interconnect information in Table 3 1 are based on Honeywell Engineering Bulletin EB7021522 Revision A For specific avionics wiring information refer to the wiring diagrams in the FALCON 900EX aircraft maintenance manual 22 05 21 Sep 1 1996 Use o
35. 49 C190J1C 48 C190J1C 64 C190J1C 63 an ww anan imm no Po no Po no Po Po fH FSH FH FH FH NAV DATA TRM RDY RS 422 XMTR NAV DATA IN RS 422 RCVR L L L NAV CLR TO SEND ee H L fen L ee L Re L wwe wwe wwe RS 422 RCVR NAV CLK IN RS 422 RCVR PERF DATA OUT RS 422 XMTR PERF DATA TRM RDY RS 422 XMTR wwe wwe B B B B B B B B B B B B B B wwe 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont CONTROL DISPLAY UNIT CDU NO 2 cont CD 810 Function Connector Pin Connects To PERF DATA IN C120J1 c RS 422 RCVR d PERF CLR TO SEND RS 422 RCVR PERF CLK IN RS 422 RCVR C190J1B 42 SPARE SPARE R PHOTO SENSOR OUT L PHOTO SENSOR OUT SPARE DIM CALIBRATION SPARE LAMP TEST GND OPEN FIGURE 8 7 SPARE SPARE ANNUN DIMMING ENABLE FIGURE 8 6 28V 0PEN ANNUN INTENSITY CONTROL FIGURE 8 7 0 28 V SPARE SPARE SPARE SPARE SPARE SPARE COLOR MONO TEST ENABLE GND OPEN SPARE SPARE GG SPARE C120J1 HH 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3
36. 49 Config 48 No MLS 0 Single MLS 0 Dual MLS 1 Triplex MLS 1 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont UTC Clock Control Internal to IAC 3 Discretes UTC Clock Control Internal to IAC Config 52 Config 51 Config 50 Priority FMS Controls the UTC Clock FWC Controls the UTC Clock Priority External Clock Controls the UTC Priority Priority Priority RPrRrRrOoOOO oO PrROOrFrr OO For the Priority cases priority scheme is used to select the source of clock control The order of priority from highest to lowest is External Clock FMS and FWC All sources are examined from highest priority to lowest The first valid source encountered is used to control the clock IAC Transmits WX Control via RS 422 IAC Transmits WX Control via RS 422 Config 53 No WX Control via RS 422 0 WX Control via RS 422 1 Dual Rad Alt Installed Dual Rad Alt Installed Config 54 Single Rad Alt 0 Dual Rad Alt 1 Cat II ILS Enabled 1 Discrete Cat II ILS Enabled Config 55 Cat II ILS Not Enabled 0 CAT II ILS Enabled 1 Cat II MLS Enabled 1 Discrete Cat II MLS Enabled Config 56 Cat II MLS Not Enabled 0 CAT II MLS Enabled 1 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the
37. 58 E135J1 51 C115J1 58 28 V DC POWER FIGURE 8 6 1 DAU 2 REV GND OPEN E135J1 52 C115J1 60 1 DH MDA GND OPEN 1103 4 C115J1 61 SPARE SPARE SPARE SPARE 1103 2 MIN SEL KNOB C115J1 66 1103 3 C115J1 67 HDG TRK KNOB CRS KNOB SPARE KNOB SPARE KNOB 115J1 75 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 1 CONT DC 840 Function Connector Pin 0 5 V DC EDGE 115J1 76 22 LIGHTING L 77 22 BO 78 24 Bl 115J1 79 24 TAS MACH KNOB TAS MACH SEL PB 115J2 1 24 GND OPEN TAS MACH MAN FMS SW 2 GND OPEN FGC SEL 1 2 PB GND OPEN 3 ASEL 100 1000 FT SW GND OPEN RAD ALT REV 1 GND OPEN RAD ALT REV 2 GND OPEN SPARE PB GND OPEN DU 1 PBO RESERVED GND OPEN DU 1 1 RESERVED GND OPEN DU 1 PB2 FPA GND OPEN DU 1 PB3 METRIC GND OPEN DU 1 PB4 IN HPA GND OPEN DU 1 PB5 RESERVED 13 GND OPEN SPARE PB GND OPEN 115J2 14 Connects To FIGURE 8 7 LIGHTING GND C115J1 78 1103 9 C115J1 79 1103 12 C115J2 1 1103 10 C115J2 2 1103 13 C115J2 3 1103 7 C115J2 4 13531 18 C115J2 5 C135J1 18 C115J2 6 130J1 60 C115J2 9 130J1 51 C115J2 10 130J1 50 C115J2 11 130J1 47 C115J2 12 22 05 21 Sep 1 1
38. 97 123J1 K CLOCK OUT 190J1A 97 E190J1A 97 FMS RS 422 TX L 98 123 1 G L GND 190J1A 98 E190J1A 98 308 24 seen sees SPARE H 429 XMTR 6 L 101 24 FIGURE OTe GND GC PANEL BUTTON ARM 100 24 1142 47 GND OPEN 101 SEE C190J1A 99 YD DISCONNECT OPEN GND 102 24 SIGNAL GROUND FGC RESERVED 103 TRIM RATE CMD OUT 104 TRIM RATE CMD OUT LCL 105 CROSS YD PWR C190J1A 106 24 190J1C 4 SENSE IN 28 V OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 Function Connector Pin Connects To SPARE FMS DISC IN C190J1B 1 GND OPEN YD POWER RETURN 2 YD POWER RETURN 3 DC POWER GND 28 VDC AIRCRAFT L 4 RAM BATTERY H zb FWC RESET GND OPEN 6 FGC RESERVED 7 28V YD SERVO POWER 8 28V YD SERVO POWER 9 FIGURE 8 6 PITCH WHEEL 1 S T S 1131 44 190J1B 10 PITCH WHEEL 1 H 11 24 1101 43 SPARE FMS DISC 12 190J1B 11 GND OPEN ASCB NO 1 PRI H 13 ASCB NO 1 PRI L FIGURE 8 1 GND L GND SEE C190J1B 13 RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED WX 2 RANGE UP O
39. ASCB CABLE OR ELECTRICAL EQUIVALENT AD 21675 R3 NOTES IAC DU Bus Interface Unterminated DU Figure 6 1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont If termination resistors in the aircraft wiring are undesirable each DU has provisions for bus termination The high H or and low L or inputs are always used To terminate a bus at a given DU install a 6 inch maximum 24 AWG jumper wire between the L input and the TERM input as shown in Figure 6 2 and Figure 6 3 NOTE If a terminating DU is removed from the panel all remaining DUs utilizing that particular bus may fail to operate or may operate intermittently DU 2KQ DU DISPLAY TERM BUS INPUT CEPE 7 AD 30104 R1 DU Display Bus Termination Provision Figure 6 2 200 MAX SG 1 MHZ BUS TERMINATED UNTERMINATED UNTERMINATED DU DU NOTES 1 THE STUB SHEILDING CAN BE ELIMINATED BY CONSTRUCTING THE STUB AS SHOWN IN FIG 5 2 CABLE ASCB CABLE OR ELECTRICAL EQUIVALENT AD 21678 R3 IAC DU Bus Interface Terminated DU Figure 6 3 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information co
40. ASEL KNOB BO 115J1 47 C115J1 47 0 ASEL KNOB Bl 115J1 48 C115J1 48 0 ASEL 100 1000 FT SWITCH 115J2 4 C115J2 4 0 IAS MACH KNOB BO 115J1 78 C115J1 78 0 IAS MACH KNOB B1 115J1 79 11501 79 0 TAS MACH MAN FMS SWITCH 115J2 2 C115J2 2 0 IAS MACH PUSH CHG BUTTON 115J1 21 C115J1 21 0 IAS MACH SEL BUTTON 115J2 1 C115J2 1 0 FGC SEL 1 2 BUTTON 115J2 3 C115J2 3 I TRIM DISENGAGE BUTTON P PUSHBUTTON GND SPARE SPARE SPARE SPARE SPARE SPARE SPARE 1143 22 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AILERON SERVO SM 200A IO BP Function Connector Pin Connects To I SERVO DRIVE 12J1 A 190J1C 1 CCW DRUM ROTATION l l C190J1C 1 1 L B 190J1C 2 G C190J1C 2 CHASSIS GND POSITION SYNCHRO REP 26 V AC 400 HZ L SERVO CLUTCH RESERVED SERVO CLUTCH H NE 13J1 G G 190J1C 12 C190J1C 12 190J1D 89 C190J1D 89 E190J1D 89 SERVO CLUTCH L DC POWER GND SERVO CLUTCH RESERVED TACH SHIELD SERVO TACH H 190J1D 59 CCW DRUM ROTATION C190J1D 59 190J1D 58 L GND C190J1D 58 SPARE SEE 12J1 L POSITION SYNCHRO OUTPUT X POSITION SYNCHRO OUTPUT Y POSITION SYNCHRO OUTPUT Z SPARE SPARE U SPARE 12J1 V 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject
41. BUS 2 SPARE WX BUS 1 WX BUS 1 NO TERM ee NO TERM L ce NO TERM L H L Connector Pin C130J1 55 56 57 59 60 61 62 C130J1 79 GND SEE C130J1 66 L_GND 22 05 21 Connects To C130J1 59 C130J1 58 115J2 23 C115J2 23 SIGNAL GND 190J1C 20 C190J1C 20 E190J1C 20 190J1C 21 C190J1C 21 E190J1C 21 C130J1 70 C130J1 69 C130J1 75 C130J1 74 FIGURE 8 14 Page 3 166 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 5 cont DU 870 10 BP Function Connector Pin Connects To 1 SIGNAL GROUND SIGNAL GND RESERVED RESERVED WX BUS 3 TERM RESERVED SPARE SPARE PORT SEL 3 GND OPEN C135J1 45 PORT SEL 2 GND OPEN C135J1 42 PORT SEL 1 GND OPEN I D 3 GND OPEN SIGNAL GND I D 2 GND OPEN 1 I D 1 GND OPEN SIGNAL GND RESERVED CHASSIS GND RESERVED RESERVED RESERVED RESERVED SOFTWARE ENABLE GND OPEN SOFTWARE ENABLE 100 GND OPEN 28 VDC POWER 101 28 VDC POWER 102 FIGURE 8 6 28 VDC POWER 103 28 VDC POWER RETURN 104 28 VDC POWER RETURN 105 DC POWER GND 28 VDC POWER RETURN C130J1 106 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM
42. BUTTON GND OPEN 53 11 R SEL BUTTON GND OPEN 54 111 DISABLE GND OPEN 55 1 RESET GND OPEN 1102 56 FIGURE 8 7 L LIGHTING GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC cont GC 810 10 BP Function Connector Pin Connects To 12 ANN VALID 28V OPEN 1102 57 24 C190J1D 14 SPARE 58 SPARE S 28V 0PEN SPARE S GND OPEN SPARE S GND OPEN SPARE S GND OPEN SPARE S GND OPEN SPARE S GND OPEN 12 L SEL BUTTON GND OPEN 65 12 R SEL BUTTON GND OPEN 66 2 DISABLE GND OPEN 67 2 RESET GND OPEN 68 SPARE 69 SPARE GND OPEN 70 12 AP DISCONNECT GND OPEN 71 FIGURE 8 11 SPARE 72 SPARE 28V 0PEN SPARE SPARE GND OPEN SPARE SPARE SPARE 78 SPARE 11 2 79 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC cont GC 810 IO BP Function Connector Pin Connects To I SIGNAL GROUND 1103 1 SIGNAL GND 0 MINIMUMS KNOB BO 2 115J1 66 C115J1 66 0 MINIMUMS KNOB B1 3 115J1 67 C115J1 67 0 MINIMUM MDA DH SWITCH 4 115J1 61 C115J1 61 0
43. Connects To LT DEEC MANUAL G O 136 2 1 RT DEEC MANUAL 06 0 2 LT FUEL FILTER BYPASS G 0 3 RT FUEL FILTER BYPASS G 0 4 CTR TANK FUEL LOW G 0 CTR TANK LOW FUEL G 0 LT ENG ANTI ICE ON 6 0 RT ENG ANTI ICE ON 6G 0 WING ANTI ICE ON 6G 0 LT BLEED OVERHEAT 6G 0 RT BLEED OVERHEAT 0 0 PASS OVERHEAT 0 0 LT PITOT HEAT OFF 0 0 CTR PITOT HEAT OFF 6 0 LT AOA HEAT OFF 0 0 WEIGHT ON LT MN GEAR G 0 FIGURE 8 5 WEIGHT ON NOSE GEAR G 0 FIGURE 8 5 WEIGHT ON RT MN GEAR 6 0 FIGURE 8 5 LANDING GEAR DOWN 6 0 CABIN DOOR OPEN G 0 BAGGAGE DOOR OPEN G 0 AFT DOOR OPEN G 0 MASTER WARNING ANN G 0 PILOT PUSH TO TALK G 0 FDR EVENT MARKER G 0 NO TAKEOFF WARNING 0 0 INBRD SLATS RETRACTED G 0 27 LT HYD PRESSURE LOW G 0 28 RT HYD PRESSURE LOW G 0 29 HF 1 SELCAL ACTIVE 6G 0 SELCAL RESET 6G 0 SPARE 0 0 SPARE 6 0 SPARE 6 0 SPARE 6 0 35 SPARE 6 0 136 2 36 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title pa
44. DIM K FIGURE 8 7 RANGE UP 190J1B 29 C190J1B 29 E190J1B 29 SHIELD GND RANGE DN 190J1B 30 C190J1B 30 E190J1B 30 FORCED SBY NO 1 GND OPEN P FIGURE 8 5 REMOTE ON GND OPEN R 5901 0 C61J1 R 190J1B 45 C190J1B 45 E190J1B 45 FORCED SBY NO 2 GND OPEN S OFF IN T C61J1 U OFF OUT 61J1 U C61J1 T 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WEATHER RADAR CONTROLLER NO 1 0 10 BP Function Connector Pin Connects To SPARE 61 3 SPARE SPARE SPARE POWER ON NO SPARE SPARE LX STBY LX ENABLE NO LX CLR TEST CTL PANEL RETURN CTL PANEL RETURN SPARE SPARE SPARE SPARE SPARE SPARE tot UJ 145J1B 66 145J1B 64 145J1B 65 145J1B 63 145J1B 61 Eod 0 dod d od gd CHAMNWDVZSCHACGCIOMmMM Moo aD w 1 This page is used only if Honeywell Lightning Sensor System is installed 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 1 DC 840 Function Connector Pin Connects To 28 V DC POWER RETURN 115J1 1 22 DC POWER GND SIGNAL GROUND 2 SIGNAL GND CHASSIS GROUND
45. DISC IN 64 GND OPEN SPARE DIO DISC IN 65 GND OPEN FGC RESERVED 66 IAC OVERHEAT GND OPEN 67 190J1D 2 C190J1D 2 E190J1D 2 PRI RADIO TUNE GND OPEN 68 SPARE DIO DISC IN 69 28V 0PEN RSB PRIMARY H 70 RSB PRIMARY L 71 SPARE FWC DISC IN 72 28V 0PEN RSB RESERVED 73 RSB RESERVED 74 AWP MASTER OUT GND OPEN 75 AURAL WARNING 76 AURAL WARNING 1 77 SPARE CARD RESERVED 78 SPARE CARD RESERVED 79 FMS INITIATE RECEIVE 80 GND OPEN FMS INITIATE TRANSFER 81 GND OPEN SPARE DIO DISC OUT 82 GND OPEN SPARE DIO DISC OUT E190J1B 83 GND OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pin Connects To I SPARE DIO DISC IN E190J1B 84 GND OPEN 1 SPARE DIO DISC IN 85 GND OPEN 1 RESERVED CROSS SIDE 86 AWP MASTER GND OPEN 1 PILOT STICKSHAKER 87 28V 0PEN SPARE DIO DISC IN 88 28V 0PEN RSB RESET GND OPEN 89 DP2 RESET GND OPEN 90 RESERVED MASTER WARNING 91 HORN GND OPEN SPARE CARD RESERVED 92 SPARE CARD RESERVED 93 CONFIG MODULE 5V POWER 94 E199J1 1 CONFIG MODULE RETURN 95 E199J1 2 CONFIG MODULE DATA RX 96 E199J1 3 SPARE DIO DISC IN 97 GND OPEN R
46. Do not tighten setscrews g Slide the PUSH TEST pushbutton onto the shaft h Align the access holes in the outer knob with the setscrews in the PUSH TEST pushbutton i Tighten the PUSH TEST pushbutton setscrews j Ensure that the space between the knob and the front panel is approximately 0 030 inch 0 8 mm k Tighten the knob setscrews I Visually check the spacing between the knob and front panel to ensure that the knob has not slipped during installation 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 22 Procedure for the RT 300 Radio Altimeter Receiver Transmitter A Removal and Reinstallation Procedures 1 Remove RT 300 a Disconnect aircraft cable and antenna connectors b Remove and set aside mounting hardware on front of unit and loosen mounting hardware on rear of unit and remove unit 2 Reinstall RT 300 a Slide unit into mounting tray and secure with applicable hardware b Mate aircraft cable and antenna connectors B Adjustment Procedures Adjustment for the Radio Altimeter Display Zero Ground NOTE There are two ways that the zero ground adjustment can be accomplished The preferred and most accurate way is described in paragraph 22 B 1 If a cable Figure 4 5 is not available to perform this procedure then the alternate procedure in paragraph 22 B 2 can be use
47. EICAS SG SEL 1 GND OPEN 16 C135J1 14 E135J1 14 EICAS SG SEL 3 GND OPEN 17 C135J1 12 E135J1 12 1 RA REV PB GND OPEN 18 115J2 5 C115J2 5 SPARE SPARE SPARE SPARE SPARE 561 NORM GND OPEN E135J1 48 SPARE SPARE SPARE SPARE SPARE SPARE SPARE 5061 REV GND OPEN 135J1 32 E135J1 47 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Honeywell Table 3 1 Interconnect Information cont REVERSIONARY CONTROLLER NO 1 cont RC 820 Function SPARE SPARE SPARE SPARE SPARE SPARE SG1 REV GND OPEN 5061 REV GND OPEN 5061 REV GND OPEN DU 1 PORT SEL 2 GND OPEN DU 3 PORT SEL 3 GND OPEN PILOT BACKED UP BY IAC 3 GND OPEN DU 1 PORT SEL 3 GND OPEN PILOT BACKED UP BY IAC 3 GND OPEN DU 2 PORT SEL 2 GND OPEN DU 2 PORT SEL 3 GND OPEN SG 1 TEST PB GND OPEN SIGNAL GROUND 1 ADC REV PB GND OPEN 1 IRS REV PB GND OPEN 5 VDC LIGHTING DC LIGHTING COMMON 28 VDC LIGHTING 50 51 52 53 54 135J1 55 SYSTEM MAINTENANCE MANUAL FALCON 900EX Connector Pin 135J1 33 34 22 05 21 Connects To C190J1D 45 E190J1D 45 190J1D 45 130J1 88 132J1 87 E135J1 18 E135J1 41 130J1 87 E135J1 46 131J1 88 131J1 87 190J1B 51 115J2 15 C115J2 15 SIGNAL GND 115J1 55 C115J1 55 115J1 54 C115J1 54 FIGURE 8 7 LIGHTING GND Page 3 71 Sep 1
48. F10 ASCB NO 1 PRI L F13 S FIGURE 8 1 RESERVED F11 RESERVED F12 F13 RESERVED F14 RESERVED 17001 15 SEE C170J1A F10 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Honeywell Function RESERVED GNSSU 1 TIME MA GNSSU 1 TIME MA RESERVED RESERVED RESERVED RESERVED RESERVED CHARGER INHIBIT RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RS 232 DATA XMT RS 232 DATA RCV RS 232 COMMON RS 232 DIR RS 232 CTS RESERVED RESERVED MEM ACCESS WR E RESERVED RESERVED RESERVED RESERVED RESERVED SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Connector Pin 170 1 61 RK 2 G2 RK 2 L G3 R R NABLE H11 H12 H13 H14 170 1 15 SEE C170J1A H3 22 05 21 14971 9 BATT CHARGER INHIBIT INPUT FIGURE 8 3 FIGURE 8 3 Page 3 179 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III 10 BP Function Connector Pin Connects To RESERVED C170J1A J1 RESERVED J2 RESERVED RESERVED RESERV
49. FALCON 900EX Table 3 1 Interconnect Information cont TAC INSTALLATION MODULE NO 2 IM 803 Function Connector Pin Connects To 5 VDC POWER C199J1 1 C190J1B 94 5 VDC POWER RETURN 2 24 C190J1B 95 DATA XMTR C199J1 3 C190J1B 96 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont SUPPLEMENTARY WIRING INFORMATION FIGURES 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 127 OHM TEST CONN NO 1 AA FIGURE 3 cc 190J1D C190J1B 104 13 106 2 15 E190J1D 4 C170J1A F10 E170J1A ki C13 4 9J1 4 30 65 sj 136 1A 4 137 2 94 94 77 34 V 127 OHM 137J2B 127 OHM AD 41489 NOTE Shielding connections assume the stub is constructed as shown in Figure 5 2 If this method of stub construction is not feasible the stub shield must be connected to ASCB bus shield at one end and connected to aircraft ground at the other end as shown in Figure 5 1 ASCB Connections Bus 1 Primary and Bus 1 Backup Figure 8 la 22 05 21 Sep 1 1996 Use or disclosure of information on this pag
50. L 39 FGC RESERVED 40 SPARE FGC DISC IN 41 28V 0PEN FGC RESERVED 42 FGC RESERVED C190J1C 43 24 s BUD cu ce FIGURE 8 2 GND S C130J1 66 190J1C 20 E190J1C 20 24a aa ES C130J1 79 GND 190J1C 21 E190J1C 21 FIGURE 8 2 FIGURE 8 2 E135J1 5 C115J1 4 GND L_GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To 0 CROSS AP PWR SENSE C190J1C 44 24 190J1A 93 OUT 28 V OPEN FGC RESERVED 45 FGC RESERVED 46 FGC RESERVED 47 FMS CDU DTR OUT i 48 S Cl120J1 V FMS RS 422 TX H 49 S C120J1 U FGC RESERVED 50 FMS CDU DATA OUT L 51 S CI20J1 T FMS RS 422 TX H 52 S T S 120 1 5 L_GND SPARE CARD RESERVED 53 SPARE CARD RESERVED 54 CROSS CHANNEL SYNC OUT 55 190J1A 92 GND OPEN SPARE FGC DISC IN 56 28V 0PEN FGC RESERVED 57 FMS CDU CTS IN k 58 S C120J1 R FMS RS 422 RX H 59 S C120J1 P SPARE FGC ANALOG IN H 60 SPARE FGC ANALOG IN L 61 FGC RESERVED 62 FMS CDU CLOCK OUT 63 C120J1 X FMS RS 422 TX 64 S C120J1 W L H H L TCAS 65 A 429 RCVR 6 66 S FIGURE 8 2 SPARE CARD RESERVED 67 SPARE
51. OPEN 12 135J1 17 E135J1 12 AUTO EICAS REV 1 GND OPEN 13 24 135J1 15 E135J1 17 AUTO EICAS REV 2 GND OPEN 14 24 135J1 16 E135J1 14 EICAS SG SEL 2 GND OPEN 15 135J1 13 E135J1 16 EICAS SG SEL 1 GND OPEN 16 135J1 14 E135J1 23 EICAS SG SEL 3 GND OPEN 17 135J1 12 E135J1 13 2 RA REV PB GND OPEN 18 115J2 6 C115J2 6 SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE 31 SPARE C135J1 32 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont REVERSIONARY CONTROLLER NO 2 cont RC 820 Function Connector Pin Connects To SPARE C135J1 33 SPARE 34 SPARE SPARE SPARE SPARE SG2 REV GND OPEN 4 C190J1D 29 SG2 REV GND OPEN E190J1D 29 SG2 REV GND OPEN 190J1D 29 DU 5 PORT SEL 2 GND OPEN 42 C130J1 88 SPARE 43 COPILOT BACKED UP BY IAC 3 44 E135J1 40 GND OPEN DU 5 PORT SEL 3 GND OPEN 45 C130J1 87 COPILOT BACKED UP BY IAC 3 46 E135J1 45 GND OPEN DU 4 PORT SEL 2 GND OPEN 47 C131J1 88 DU 4 PORT SEL 3 GND OPEN 48 131 1 87 SG 2 TEST PB GND OPEN 49 C190J1B 51 115J2 16 C115J2 16 SIGNAL GROUND 50 SIGNAL GND 12 ADC REV PB GND OPEN 51 115J1 57 C115J1 57 2 IRS REV PB GND OPEN 52 115J1 56 C115J1 56 5 VDC LIGHTING 53 FIGURE 8
52. OUT RADALT IN RADALT VALID RADALT VALID RADALT TEST IN RADALT TEST OUT AD 41502 Single Radio Altimeter Figure 8 13 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AD 41503 69 70 C130J1 74 75 85786 la 25 ctooytA 69 70 013101 74 75 77 T8 1321 74 75 38 39 35 36 19 20 58 E 38 39 35 36 69 70 lAC3 LIII E e 6 2022 T 77 78 13141 74 75 69 70 19 20 58 38 39 35 36 19 20 58 59 77 78 1301 LlI l 74 75 rep 69 70 IAC 1 E B5 6 2 25 19ojtA NOTE Shielding connections assume the stub is constructed as shown in Figure 5 2 If this method of stub construction is not feasible the stub shield must be connected to bus shield at one end and connected to aircraft ground at the other end as shown in Figures 6 1 6 3 6 4 and 6 6
53. Reinstall SB 201 a Mount drum and bracket assembly rigidly to airframe with four 1 4 inch diameter bolts of sufficient length and four suitable lock washers and nuts 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX INSTALLATION CRITICAL TO ENSURE CABLE TERMINAL CAPTURE USE ONLY 0 138 32 NC 2A STAINLESS STEEL DRILLED SCREWS HONEYWELL PART NO 2554911 1 STANDARD FILLISTER HEAD SCREWS MAY NOT PROPERLY RETAIN THE CABLE TERMINAL b Wrap bridle cables around servo bracket drum Secure swaged cable terminals to servo bracket drum with screws removed in paragraph 23 A 3 e or if new servo use screws supplied with new servo Safety wire screws through adjacent holes in drum with Low Mu Monel wire 0 020 inch diameter and 4 inches long c Adjust control system and bridle cables to proper tension as instructed in the aircraft maintenance manual INSTALLATION CRITICAL TO ENSURE THAT THE CABLE CANNOT JAM BETWEEN THE DRUM AND KEEPERS THE DISTANCE BETWEEN THE KEEPERS AND DRUM SHALL BE MEASURED AFTER THE KEEPERS AND RETAINING PLATE ARE INSTALLED THE DISTANCE BETWEEN THE DRUM AND KEEPERS SHALL NOT EXCEED 0 040 INCH AND SHALL NOT BE LESS THAN 0 005 INCH THE 3 32 INCH CABLE DIAMETER SHALL BE VERIFIED THESE ARE CRITICAL INSTALLATION REQUIREMENTS d Install two of four cable keepers removed in paragr
54. SIGNAL GND SDI 3 GND OPEN SPARE WOW GND OPEN FIGURE 8 5 SIGNAL GROUND SIGNAL GND SPARE SPARE GND OPEN SPARE GND OPEN GND OPEN GND OPEN 28 V OPEN 28 V OPEN KNOTS GND OPEN KNOTS GND OPEN KNOTS GND OPEN TO AIRCRAFT KNOTS GND OPEN TAS KNOTS GND OPEN 28 VDC POWER FIGURE 8 6 28 VDC POWER RETURN 27 DC POWER GND I I I HH ww 2 2 2 I IV OVERSPEED WARNING DISC 28 OVERSPEED HORN GND OPEN MADC VALID DISC GND OPEN 29 ASCB NO 2 PRI H 0 ASCB NO 2 PRI L C9J1 34 FIGURE 8 1 GND L GND w wwe 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont MICRO AIR DATA COMPUTER MADC NO 2 cont AZ 840 10 BP Function Connector Pin Connects To I TEMPERATURE PROBE H C9J1 31 24 5 S T S 500 OHM l l TEMPERATURE 1 TEMPERATURE PROBE 1 32 24 PROBE G SPARE 33 34 AOA POTENTIOMETER 35 ANGLE OF AOA POTENTIOMETER W 36 ATTACK AOA POTENTIOMETER L 37 POTENTIOMETER CALIBRATION ENABLE 38 GND OPEN SPARE 39 SPARE 40 ATC SELECT GND OPEN ATC Al ATC ATC ATC ATC ATC ATC ATC ATC ATC SP
55. connector Use a 50 pin mating connector to fabricate a small harness See Figure 4 2 for a diagram of the harness 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX c Attach the harness to the test connector and connect the test harness batteries NOTE The test harness batteries will be used to maintain the RAM power during battery exchange which will avoid loss of data d Separate the small connector from the IAC and use the connector and wires to slowly extract the battery from the computer 50 PIN CANNON D MALE PINS e WITH PENLIGHT SIZE IAC BATTERY HOLDER TEST BATTERY AND THREE 3 CONNECTOR PACK AA ALKALINE FRONT BATTERIES 1N4148 OR EQUIVALENT OR EQUIVALENT AD 41117 Figure 4 2 IC 800 IAC Test Connector Harness 3 Install new battery a Install a new battery Honeywell Part Number 7014664 902 and reinstall the connector b Check and record the replacement battery voltage by probing the pins at the connector as described in paragraph 13 C 1 b c Make sure that the battery connector fits in the recessed slot and reinstall and secure the battery cover d Apply your quality inspection tamper evident seal to one of the screws on the top of the battery cover e Remove the test connector harness and reinstall the test connector plate and hardwa
56. cont SINGLE AIRCRAFT GROUNDING POINT gt CENTRAL AIRCRAFT GND DC PWR SIGNAL LIGHTING BLOCKS GNDS GNDS GNDS Because signal grounds are low currents multiple signal grounds can be connected to remote aircraft terminal blocks other than the central grounding blocks as long as these remote terminal blocks are isolated from ground The various remote signal ground blocks must all be grounded only at the aircraft central grounding point For example if ten signal grounds are connected to a remote terminal block a minimum of one grounding wire must be run from this terminal block to the aircraft central grounding point TO VARIOUS AIRCRAFT LOCATIONS AD 34766 R1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont Grounding for F 900 See Figure 4 1 Single Shielded Cables Except Audio The shields of analog not audio cables will be gathered together with other similar shields at the signal source end of each cable A single 20 AWG pig tail will connect the group of shields to airframe using the LRU local earth post The length of the pig tail must not exceed six inches Twisted Shielded Pairs Balanced Differential Except Audio The shields for these cables will be grounded at both ends of the cable by gathering the screens a
57. data base information on disc 2 Through the use of the DL 900 Data Loader you have the option to transfer the custom database to 3 5 inch floppy diskettes Also you have the option to transfer the custom or navigation database from disc to the IAC A Removal and Reinstallation Procedures 1 Remove IC 800 IAC a Loosen the mounting tray hold down knob b Slowly pull forward on the unit handle to separate the unit and tray connectors and slide the unit out of the tray 2 Reinstall IC 800 IAC CAUTION WHEN PLACING THE UNIT ON THE MOUNTING TRAY DO NOT FORCE FIT IF MATING IS DIFFICULT REMOVE THE UNIT AND CHECK FOR CONNECTOR PINS THAT MAY BE BENT OR OUT OF ALIGNMENT ALSO VISUALLY CHECK THE ALIGNMENT OF THE RECEPTACLE ON THE MOUNTING TRAY a Slide the unit into the mounting tray b Slide the unit backwards until its connectors are fully engaged with the mating connectors of the mounting tray c If necessary gently lift the front of the unit to ensure that the hold down assembly mates properly with the tray hold down hooks d Tighten the hold down knob 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX B Data Load and Data Transfer Procedures 1 Loading the Navigation Database from the DL 900 Data Loader NOTE Every 28 days the FMS navigation database in the IC 800 IAC must
58. in pitch and roll to 0 2 degree with respect to the airframe The leveling fixture may now be removed from the mounting tray g Install the IRU in the mounting tray in accordance with paragraph 15 A 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 2 Optional Mechanical Leveling Procedure Method 2 a b 9 Perform steps in paragraph 18 B 1 a b and Check the circular level of the leveling fixture Adjust the level of the mounting tray by installing shims as required to have the bubble in the circular level inside of the second ring refer to Figure 4 4 The mounting tray will be level to within 0 2 degrees with respect to the airframe Using the thumbwheel adjustments adjust the tubular level which is perpendicular to the longitudinal axis of the aircraft the roll tubular level until the bubble is centered NOTE The sensitivity of the tubular level is 20 arc seconds per division Raise or lower the nose of the airplane at least 1 degree Note the position of the bubble in the tubular level The bubble should be within one division of the center starting position If the bubble has moved more than one division adjust the mounting tray by rotating the tray to take out one half of the change in the position of the bubble Note the position of the bubble in the tubu
59. in place by tightening the two thumb wheel clamps over the support hooks B Adjustment Procedure Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Hone ell MAINTENANCE W MANUAL FALCON 900EX 16 Procedure for the IRU Mounting Tray Fan Filter NOTE In a new installation the filter should be cleaned or replaced after approximately 100 hours of operation and then approximately every 300 hours to 500 hours depending on the environmental conditions A Removal and Reinstallation Procedures 1 Remove filter Pull up on the removal tab to separate filter from the fan 2 Reinstall filter Align the cutout area on the bottom of the filter with the wires on the fan and press down on the filter until it snaps into place B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 17 Procedure for the IRU Mounting Tray Fan NOTE Refer to Figure 4 3 when performing the procedures for IRU Mounting Tray Fan FAN HOUSING MOUNTING TRAY MACHINE SCREW 3 PL AND RIM CLAMP NOTE FAN FILTER NOT SHOWN SNAPS ON TOP AD 49488 Figure 4 3 IRU Mounting Tray Fan Housing A
60. restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont LBS KGS Selected for Display 1 Discrete LBS KGS Selected for Displa Config 57 LBS Selected for Display 0 KGS Selected for Display 1 Slip Skid Enabled 1 Discrete Slip Skid Enabled Config 58 Slip Skid Not Enabled 0 Slip Skid Enabled 1 Default ASCB Sensor Types Ignored by FMS 1 Discrete Default ASCB Sensor Types Ignored by FMS Config 59 Default Sensor Types Not Ignored 0 Default Sensor Types Ignored 1 When Config 59 0 the default sensor types config 34 37 are used and failure indications are defined from these discretes When Config 59 1 the default sensor types config 34 37 are not used and a generic sensor type is used This discrete is used by FMS only ACARS Installed 1 Discrete ACARS Installed Config 60 ACARS Not Installed 0 ACARS Installed 1 At Installed in this IAC 1 Discrete AT Installed in this IAC Config 61 AT Not Installed in this IAC 0 AT Installed in this IAC 1 Center Fuel Tank Temp Enabled 1 Discrete Center Fuel Tank Temp Enabled Config 64 Center Fuel Temp Not Enabled 0 Center Fuel Temp Enabled 1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect In
61. separation of ASCB is required in that case This requirement is deemed INSTALLATION CRITICAL 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont To ensure the required integrity of the ASCB System the ASCB buses shall be separated such that no single 12 fire axe or projectile can simultaneously cut all 4 buses This requirement is deemed INSTALLATION CRITICAL To ensure the required integrity of the ASCB System dual bus users are connected via a bus coupler to one bus DAU connected to the cross side backup bus To satisfy the 12 fire axe requirement given above and minimize bus reflections the bus coupler shall be located as close to the user as possible while maintaining 12 separation from at least one other bus This requirement is deemed INSTALLATION CRITICAL SUBSYSTEM N CABLE RAYCHEM 2524E0114 OR FILOTEX 69654 1279 THERMORAD JACKET NOTES 1 THE STUB SHIELDING CAN BE ELIMINATED BY CONSTRUCTING THE STUB AS SHOWN IN FIG 5 2 AD 32182 R1 ASCB Bus Construction Figure 5 1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont CHASSIS GROU
62. this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont FMS Not Installed in this IAC FMS Not Installed in this IAC Config 9 FMS Installed in this IAC 0 FMS Not Installed in this IAC 1 1 of FMS s Installed 2 Discretes dt of FMS s Installed Config 11 Config 10 No FMS 0 Single FMS 0 Dual FMS 1 Triplex FMS 1 A429 LRN 1 Configuration 3 Discretes A429 LRN 1 Configuration Config 17 Config 16 Config 15 Spare Low Speed IRS High Speed Omega Low Speed Spare High Speed GPS Low Speed GPS High Speed Spare High Speed Spare Low Speed RPrRrRrROOO oO r3 L0 A429 LRN 1 Number 2 Discretes A429 LRN 1 Number Config 19 Config 18 LRN 0 0 LRN 1 0 LRN 2 1 LRN 3 1 Dual Single Autopilot Installed 1 Discrete Dual Single Autopilot Installed Config 20 Dual Autopilot Installed 0 Single Autopilot Installed 1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AFIS Installed 1 Discrete AFIS Installed Config 21 AFIS Not Installed 0 AFIS Installed 1 A429 LRN 2 Configuration 3 Discretes A429 LRN 2 Configuration Config 24 Config 23 Conf
63. to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont ELEVATOR SERVO SM 200A 10 BP Function Connector Pin Connects To I SERVO DRIVE H 13J1 A 190J1C 3 CCW DRUM ROTATION l l C190J1C 3 I L B 190J1C 5 G C190J1C 5 CHASSIS GND POSITION SYNCHRO REP 26 V AC 400 HZ L SERVO CLUTCH RESERVED SERVO CLUTCH H NE 12J1 G G 190J1C 12 C190J1C 12 190J1D 89 C190J1D 89 E190J1D 89 SERVO CLUTCH L DC POWER GND SERVO CLUTCH RESERVED TACH SHIELD SERVO TACH H 190J1D 61 CCW DRUM ROTATION C190J1D 61 190J1D 60 L GND C190J1D 60 SPARE SEE 13J1 L POSITION SYNCHRO OUTPUT X POSITION SYNCHRO OUTPUT Y POSITION SYNCHRO OUTPUT Z SPARE zT SPARE U SPARE 13J1 V 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont RUDDER LINEAR ACTUATOR SM 725 10 BP Function Connector Pi Connects To 1 MOTOR EXTEND 14J1 A 190J1C 26 l l C190J1C 26 1 INPUT RETRACT B 190J1C 13 G C190J1C 13 0 CENTERING EXTEND C 190J1D 16 C190J1D 16 0 SWITCH RETRACT D 190J1D 17 C190J1D 17 0 CENTERING SWITCH COM R DC POWER GND 1 22 S S 190J1C 10 190J1D 91 C190J1D 91 E190J1D 91 GND L_G
64. 1 0 3 94 0 3 142 0 3 95 0 3 143 0 3 96 0 3 144 0 3 97 0 3 145 0 3 98 0 3 146 0 3 99 0 3 147 0 3 100 0 3 148 0 3 101 0 3 149 0 3 102 0 3 150 0 3 103 0 3 151 0 3 104 0 3 152 0 3 105 0 3 153 0 3 106 0 3 154 0 3 107 0 3 155 0 3 108 0 3 156 0 3 109 0 3 157 0 3 110 0 3 158 0 3 111 0 3 159 0 3 112 0 3 160 0 3 113 0 3 161 0 3 114 0 3 162 0 3 115 0 3 163 0 3 116 0 3 164 0 3 117 0 3 165 0 3 118 0 3 166 0 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX SUBHEADING AND PAGE REVISION SUBHEADING AND PAGE REVISION Section 3 cont 3 213 0 System Interconnects 3 214 0 3 167 0 3 215 0 3 168 0 3 216 0 3 169 0 3 217 0 3 170 0 3 218 0 3 171 0 3 219 0 3 172 0 3 220 0 3 173 0 3 221 0 3 174 0 3 222 0 3 175 0 3 223 0 3 176 0 3 224 0 3 177 0 3 225 0 3 178 0 3 226 0 3 179 0 3 227 0 3 180 0 3 228 0 3 181 0 3 229 0 3 182 0 3 230 0 3 183 0 3 231 0 3 184 0 3 232 0 3 185 0 3 233 0 3 186 0 3 234 0 3 187 0 3 235 0 3 188 0 3 236 0 3 189 0 3 237 0 3 190 0 3 238 0 3 191 0 3 239 0 3 192 0 3 240 0 3 193 0 3 241 0 3 194 0 3 242 0 3 195 0 3 243 0 3 196 0 3 244 0 3 197 0 3 198 0 Table of Contents Section 4 3 199 0 TC4 1 0 3 200 0 TC4 2 0 3 201 0 3 202 0 Section 4 3 203 0 Maintenance Practices 3 204 0 4 1 0 3 205 0 4 2 0 3 206 0 4 3 0 3 207 0 4 4 0 3 208 0 4 5 0 3 209 0 4 6 0 3 210 0 4 7 0 3
65. 131J1 28 SEE C131J1 29 RESERVED RESERVED BUS 4 TERM DU 4 PB5 RIGHT PB 115J1 52 GND OPEN C115J1 52 DU 4 PB4 115J1 51 GND OPEN C115J1 51 RESERVED BUS 2 TERM 49 DU 4 PB3 50 115J1 50 GND OPEN C115J1 50 DU 4 PB2 51 115J1 49 GND OPEN C115J1 49 BUS 1 TERM 52 REM LT SENSOR PWR H 53 REM LT SENSOR PWR L C131J1 54 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 4 cont DU 870 Function Connector Pin Connects To RESERVED C131J1 55 RESERVED 56 RESERVED 57 BUS 4 58 H BUS 4 NO TERM L 59 FIGURE 8 14 DU 4 1 60 115J1 44 GND OPEN C115J1 44 WX BUS 2 TERM 61 DU 4 PBO LEFT PB 62 115J1 43 GND OPEN C115J1 43 KNOB PB COMMON 63 SIGNAL GND WX BUS 1 TERM 64 DU OVERTEMP GND OPEN 65 DU WRAPAROUND H 66 190J1A 16 A 429 XMTR C190J1A 16 E190J1A 16 L 79 5 5 190J1A 15 C190J1A 15 E190J1A 15 RESERVED 67 RESERVED 68 WX BUS 3 69 C131J1 70 WX BUS 3 NO TERM L L 70 C131J1 69 RESERVED 71 RESERVED 72 RESERVED 73 WX BUS 2 m 74 C131J1 75 WX BUS 2 NO TERM L 75 C131J1 74 SPARE 76 WX BUS 1 Ia 77 WX BUS 1 NO TERM 1 C13101 78 FIGURE 8 14 GND Lend 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subj
66. 13J1 A C190J1C 3 13J1 B C190J1C 5 C190J1A 106 FIGURE 8 9 FIGURE 8 9 14J1 E C190J1C 10 190J1D 91 C190J1D 91 E190J1D 91 12J1 G 13J1 G C190J1C 12 190J1D 89 C190J1D 89 E190J1D 89 14J1 B C190J1C 13 14J1 A C190J1C 26 FIGURE 8 2 3 121 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 Function Connector Pin Connects To H 190J1C 16 24 S t 17 24 Ge FIGURE 8 2 GND 18 24 S AFIS H A 429 RCVR 14 19 24 FIGURE 85 DU 5 WRAPAROUND 220 C24 ie ae eee S T S C130J1 66 A 429 RCVR 13 C190J1C 20 E190J1C 20 L 21 24 25622525255 C130J1 79 GND C190J1C 21 E190J1C 21 LRN 3 A 429 RCVR 16 H L H L H SPARE FGC DISC IN 22 GND OPEN SPARE FGC DISC IN 23 GND OPEN SPARE L 24 A 429 RCVR 18 Fr 25 S T S FIGURE 8 2 26 SPARE CARD RESERVED 27 MLS 1 H 28 A 429 RCVR 4 be 29 S T S FIGURE 8 2 EICAS LEFT SEL 30 E135J1 7 GND OPEN PFD 1 OFF GND OPEN 31 135J1 11 AURAL WARNING OUT 32 AURAL WARNING OUT B L 33 RSB RESERVED 34 RSB RESERVED 35 RSB SECONDARY H 36 RSB SECONDARY L 37 DISPLAY CONTROL
67. 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont REVERSIONARY CONTROLLER NO 3 RC 841 Function Connector Pi Connects To EICAS E135J1 1 132J1 1 BRIGHTNESS POT W 2 L 3 DU 3 OFF GND OPEN 4 E135J1 8 EICAS LEFT SEL GND OPEN 5 C190J1C 30 EICAS LEFT SEL GND OPEN 6 E190J1C 30 EICAS LEFT SEL GND OPEN 7 190J1C 30 DU 3 OFF GND OPEN 8 E135J1 4 132J1 22 EICAS C190J1B 49 E190J1B 49 190J1B 49 EICAS EICAS RIGHT SEL RIGHT SEL RIGHT SEL GND OPEN GND OPEN GND OPEN EICAS SEL LT SG GND OPEN EICAS SEL RT SG GND OPEN EICAS LT SG SEL GND OPEN EICAS PORT SEL 2 GND OPEN EICAS RT SG SEL 1 GND OPEN EICAS LT SG SEL 2 GND OPEN EICAS PORT SEL 3 GND OPEN SPARE SPARE SPARE SPARE EICAS SEL RT SG 2 GND OPEN SPARE SPARE SPARE SPARE SPARE SPARE SPARE 9 10 11 12 13 14 15 16 17 18 0 SPARE E135J1 31 22 05 21 135J1 17 C135J1 12 135J1 12 C135J1 17 135J1 16 C135J1 14 132J1 88 135J1 13 C135J1 15 135J1 15 C135J1 13 135J1 43 132J1 87 135J1 14 C135J1 16 Page 3 72 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3
68. 1C 70 OPEN GND E190J1A 17 TAG SYNC IN 3 18 190J1A 18 OPEN GND E190J1C 70 CDU SYNC IN 1 19 190J1C 69 OPEN GND F190J1A 19 GENERAL BUS 1 H 20 A 429 XMTR 1 CE C190J1A 21 FIGURE 8 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 Function Connector Pin Connects To SPARE CARD RESERVED C190J1A 22 SPARE CARD RESERVED 23 DU BUS TX 2 24 DU BUS TX 2 1 25 FIGURE 8 14 LRN 2 H 26 A 429 RCVR 15 L 27 FIGURE 8 2 DU 3 WRAPAROUND L 28 132J1 79 A 429 RCVR 11 190J1A 28 E190J1A 28 29 132J1 66 G 190J1A 29 E190J1A 29 SPARE H 30 IOP RS 422 RX L 31 CDU SYNC IN 3 32 190J1A 32 GND OPEN E190J1C 69 SPARE FMS DISC IN 33 GND OPEN SPARE FMS DISC IN 34 GND OPEN SPARE FWC DISC IN 35 GND OPEN WX CONTROL DATA 1 L 36 59J1 n IOP RS 422 RX 190J1A 36 E190J1A 36 H 37 59J1 m G 190J1A 37 E190J1A 37 SPARE CARD RESERVED 38 SPARE CARD RESERVED 39 MLS 2 H 40 A 429 RCVR 22 1 41 S T S FIGURE 8 2 DU 2 WRAPAROUND H 42 131J1 66 A 429 RCVR 10 190J1A 42 E190J1A 42 L C190J1A 43 131J1 79 G 190J1A 43 E190J1A 43 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject
69. 1D 48 SPARE DIO DISC OUT 49 28V 0PEN GC PANEL STROBE OUT L GC PANEL STROBE OUT H S 1142 5 L_GND FGC RESERVED SG 3 REV GND OPEN E135J1 42 YD LVDT FEEDBACK n 14J1 M l 190J1D 54 YD LVDT FEEDBACK H 14J1 N 190J1D 55 SPARE FGC RVDT ANALOG IN F 12J1 N L H AILERON TACH 190J1D 58 12J1 L 190J1D 59 L 13J1 N ELEVATOR TACH 190J1D 60 H 61 13J1 L G 190J1D 61 GC PANEL L 62 11J2 8 BUTTON DATA H 63 S T 1142 7 AWP ENABLE 28V 0PEN 64 SPARE FGC DISC IN 65 28V 0PEN BC ID 1 GND OPEN C190J1D 66 H 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 Function Connector Pin Connects To SPARE FMS DISC OUT C190J1D 67 GND OPEN FMS HORN FIGURE 8 15 GND OPEN SWITCHED 14J1 V LVDT RVDT l 190J1D 69 EXCITATION 14J1 U LGND 190J1D 70 RESERVED HDLC RX 1 H RESERVED HDLC RX 1 L FGC RESERVED FGC RESERVED CROSS SERVOS OFF 28V 0PEN 75 190J1A 90 CROSS SERVOS PWR OFF 76 190J1A 91 28V 0PEN AIL RVDT SURFACE POS 77 AIL RVDT SURFACE POS 78 BC ID 3 GND OPEN 79 IOP RS 232 COMMON 80 IOP RS 232 DATA XMTR 81 FIGURE 8 3 10 RS 232 DATA RCVR 82 RESERVED HDLC RX 2 H 83 RESERVED HDLC RX
70. 2 115J1 66 1103 3 115J1 67 Page 3 158 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE MANUAL FALCON 900EX Honeywell Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 2 CONT DC 840 Function 0 5 V DC EDGE LIGHTING Connector Pin H C115J1 76 22 L 77 22 BO 78 24 Bl C115J1 79 24 TAS MACH KNOB TAS MACH SEL PB C115J2 1 24 GND OPEN TAS MACH MAN FMS SW 2 GND OPEN FGC SEL 1 2 PB GND OPEN 3 ASEL 100 1000 FT SW GND OPEN RAD ALT REV 1 GND OPEN RAD ALT REV 2 GND OPEN SPARE PB GND OPEN DU 1 PBO RESERVED GND OPEN DU 1 1 RESERVED GND OPEN DU 1 PB2 FPA GND OPEN DU 1 PB3 METRIC GND OPEN DU 1 PB4 IN HPA GND OPEN DU 1 PB5 RESERVED GND OPEN SPARE PB GND OPEN 115 2 14 22 05 21 FIGURE 8 7 LIGHTING GND 1103 9 115J1 79 1103 12 115J2 1 1103 10 115J2 2 1103 13 11572 3 1103 7 115J2 4 1351 18 115J2 5 C135J1 18 115J2 6 130J1 60 115J2 9 130J1 51 115J2 10 130J1 50 115J2 11 130J1 47 115J2 12 Page 3 159 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROL
71. 25 S FIGURE 8 2 SEC IRS FMC IN 26 429 27 FIGURE 8 2 ATR GROUND 28 FIGURE 8 5 GNSSU OUTPUT 3 29 ARINC 429 30 S FIGURE 8 2 CMC IN 31 ARINC 429 32 CHASSIS GROUND 33 DC POWER GND 34 DC POWER GND 28 VDC POWER 35 FIGURE 8 6 36 SEE C149J1 5 37 SEE C149J1 18 GNSSU OUTPUT 1 H 38 ARINC 429 L 39 FIGURE 8 2 DADC IN 419 429 SELECT 40 C149J1 41 SEE C149J1 23 ANTENNA C1490 2 1 TOAS RRR iian a 0 GPS ANTENNA ANTENNA C149J2 2 L GPS ANTENNA PIC WIRE AND CABLE PART NO T556124 FOR 13 FT LENGTH FOR SMALLER SECTION USE PART NO SF 5224 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 LASEREF III Function Connector Pin Connects To IDENT RESISTOR R1 C170J1A A1 RESERVED A2 RESERVED RESERVED RESERVED RESERVED 6 SDI 4 GND OPEN FIGURE 8 4 RESERVED 8 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED IDENT RESISTOR R2 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 170 1 15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this docu
72. 29 RCVR 20 SPARE FWC DISC 82 28V 0PEN FMS DATA LOADER L 83 DTR OUT FMS RS 422 TX H 84 FGC RESERVED 85 SPARE FGC DISC IN 86 GND OPEN AT DISCONNECT OPEN GND 87 FIGURE 8 11 TRIM DISCONNNECT OPEN GND 88 FGC RESERVED E190J1A 89 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP 1 1 1 1 1 1 Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 Function CROSS SERVOS OFF IN 28V 0PEN CROSS SERVO PWR OFF IN 28V 0PEN CROSS CHANNEL SYNC IN GND OPEN CROSS AP PWR SENSE IN 28 V OPEN DU 1 WRAPAROUND H A 429 RCVR 9 L FMS DATA LOADER CLOCK OUT FMS RS 422 TX L SPARE H A 429 XMTR 6 L GC PANEL BUTTON ARM GND OPEN AT DISCONNECT B OPEN GND FGC RESERVED TRIM RATE CMD OUT H TRIM RATE CMD OUT LCL CROSS YD PWR SENSE IN 28 V OPEN Connector Pin E190J1A 90 91 92 93 94 95 Connects To 130J1 66 190J1A 94 C190J1A 94 130J1 79 190J1A 95 C190J1A 95 SEE E190J1A 6 E190J1A 47 24 S T S 99 24 S T 101 24 S T 100 101 SEE 19001 99 102 24 103 104 105 E190J1A 106 22 05 21 123J1 K 190J1A 97 C190J1A 97 123 1 190J1A 98
73. 2J1 j FIGURE 8 7 LIGHTING GND FIGURE 8 4 SIGNAL GND 170J1B A10 170J1B E3 170J1B E1 170J1B A15 170J1B F3 RO 5 Ro Ro Po annn 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO IC 800 Function SIGNAL GROUND Connector Pi 190J1A 1 28V ELEV TRIM CLUTCH OUT a IAC IDENT 2 GND OPEN FGC RESERVED 3 4 Connects SIGNAL GND SIGNAL GND ASCB NO 1 BU H 5 ASCB NO 1 BU 1 7 FIGURE 8 1 BC RS 232 DATA RCVR 6 BC RS 232 DATA XMTR 77 FIGURE 8 3 BC DL RS 232 COMMON 96 7 28 VDC AP SERVO PWR RIN 8 DC POWER GND 28 VDC AP SERVO PWR RTN 9 DC POWER GND BC RESERVED 10 28 VDC AP SERVO POWER 28 VDC AP SERVO POWER FIGURE 8 6 SPARE H IOP RS 422 TX L DU 4 WRAPAROUND L C131J1 79 A 429 RCVR 12 C190J1A 15 E190J1A 15 H C131J1 66 C190J1A 16 E190J1A 16 TAG SYNC IN 2 17 C190J1C 70 OPEN GND E190J1A 18 TAG SYNC IN 3 18 C190J1A 18 OPEN GND E190J1C 70 CDU SYNC IN 2 19 C190J1C 69 OPEN GND E190J1A 32 GENERAL BUS 1 H 20 A 429 XMTR 1 L 190 1 21 FIGURE 8 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYST
74. 3 130J1 54 REM LT SENSOR PWR H REM LT SENSOR PWR L 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP SYSTEM MAINTENANCE Honeywell MAINTE FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 1 cont DU 870 Function Connector Pin Connects To RESERVED RESERVED RESERVED BUS 4 H BUS 4 NO TERM L DU 1 PB1 FPA GND OPEN WX BUS 2 TERM RESERVED KNOB PB COMMON WX BUS 1 TERM DU OVERTEMP GND OPEN DU WRAPAROUND H A 429 XMTR L RESERVED RESERVED WX BUS 3 K WX BUS NO TERM RESERVED RESERVED RESERVED WX BUS 2 WX BUS 2 NO TERM SPARE WX BUS 1 WX BUS 1 NO TERM H L H L H L 130J1 55 56 57 130J1 59 59 130J1 58 60 115J2 9 C115J2 9 61 62 SIGNAL GND 190J1A 94 C190J1A 94 E190J1A 94 190J1A 95 190 1 95 E190J1A 95 130J1 70 130J1 69 130J1 75 130J1 74 FIGURE 8 14 GND L GND 13001 79 SEE 130J1 66 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 1 cont DU 870 10 BP Function Connector Pin Connects To 1 SIGNAL GROUND SIGNAL GND RESERVED RESERVED WX BUS 3 TERM RESERVED SP
75. 30 in 0 8 mm 6 Tighten both 6 32 set screws with the Allen wrench 7 Visually check the spacing between the knob and the bezel to make sure that the knob has not slipped during installation 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 6 Procedure for the CD 810 Control Display Unit A Removal and Reinstallation Procedures 1 Remove CD 810 Control Display Unit a Disengage the Dzus fasteners on the unit b Slide the unit out of the aircraft mounting location and disconnect the cable connector s 2 Reinstall CD 810 Control Display Unit a Mate the cable connector s with the unit connector s and slide the unit into the aircraft mounting location b Engage the Dzus fasteners on the unit B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell awe FALCON 900EX 7T Procedure for the DA 800 Data Acquisition Unit DAU A Removal and Reinstallation Procedures 1 Remove DA 800 DAU a Press up on the inside at the top of the front handle to release the locking lever Move the locking lever out and down to release the locking cam b Slowly pull forward on the handle to separate the unit and tray connecto
76. 4 1256 474932 Germany Japan Apparatebau Gauting Gmb Okura Aerospace Co Ltd Ammerseestr 45 39 6 12 Ginza 2 Chome 89317 0 Gauting Germany Chuo ku Tokyo104 Japan Tel 49 89 85601 0 Fax 49 89 85601 183 Tel 3 3566 6315 or 3 3566 6313 Fax 3 3562 4004 Australia Support Center Singapore Support Center Honeywell Ltd Honeywell Aerospace Pte Ltd Sperry Drive 2 Loyang Crescent Trade Park Singapore 1750 Tullamarine 3043 Victoria Australia Tel 65 542 1313 Fax 65 542 1212 Tel 61 3 330 1411 Fax 61 3 330 3042 Switzerland South America Jet Aviation Zurich AG TAM Taxi Aereo Marilla S A Zurich Airport Rua Monsenhor Antonio Pepe 94 P O Box 1524 Sao Paulo SP 04357 CH 8058 Zurich Switzerland Brazil Tel 41 816 4800 Tel 55 11 577 7711 ext 316 Fax 41 816 3863 Fax 55 11 533 5290 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX 6 Corporate Operations Customer Engineering Locations A United States of America U S A Western U S A Phoenix Arizona Tel 602 436 4400 Fax 602 436 4100 Los Angeles California Mobil 818 601 0626 Dallas Texas Tel 214 402 4332 Fax 214 402 4399 Seattle Washington Tel 206 656 2705 Fax 206 251 9368 Little Rock Arkansas Honeywell at Falcon Jet Tel 501 372 5254 Fax 501 372 5650 Honeywell at Rayheon Corpor
77. 6 flute Bristol wrench to loosen the setscrews in the outer knob Rotate outer knob until access hole lines up with setscrews on inner PUSH CHG pushbutton and loosen two setscrews Slide the knob and pushbutton off of the shaft Rotate knob to MAN position and loosen setscrews Slide knob off of shaft On new knobs and pushbutton make sure that the setscrews are out far enough to allow knobs and pushbutton to slide onto shaft Apply retaining compound to setscrews Slide the selector knob onto the shaft Ensure that the space between the knob and front panel is approximately 0 030 inch 0 8 mm and tighten setscrews Slide the outer knob onto the shaft Do not tighten setscrews Slide the PUSH CHG pushbutton onto the shaft Align the access holes in the outer knob with the setscrews in the PUSH TEST pushbutton Ensure PUSH CHG lettering is straight and tighten the PUSH CHG pushbutton setscrews Ensure that the two knobs are spaced approximately 0 030 inch 0 8 mm so they do not rub against each other Tighten the knob setscrews Visually check the spacing between the knobs and front panel to ensure that the knob has not slipped during installation 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 3 Replacement of the MINIMUM Knobs Rotate both knobs fully CCW Use a 0 048 inch O D 6
78. 7 DC LIGHTING COMMON 54 LIGHTING GND 28 VDC LIGHTING C135J1 55 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GLOBAL NAVIGATION SATELLITE SENSOR GNSSU NO 2 GNSSU 10 BP Function Connector Pin Connects To 0 GNSSU FAULT C149J1 1 0 RS 232 XMTR 1 RS 232 RCVR 3 FIGURE 8 3 DATA LOADER INPUT 4 ARINC 429 15 SDI 2 5 SDI 1 36 C149J1 8 PRI DADC INPUT 6 ARINC 429 7 PROG DISCRETE RETURN 8 14901 36 TIME MARK 2 9 170J1A G2 TIME MARK 2 22 S T 170J1A G3 SEC DADC INPUT 10 ARINC 429 11 DATA LOAD MODE DISCRETE 12 TIME MARK 3 H 13 E170J1A G2 TIME MARK 3 L 14 S T E170J1A G3 L_GND 15 GEN PURP INPUT 1 16 ARINC 429 17 PRI IRS FMC IN 18 _ ARINC 429 37 FIGURE 8 2 TIME MARK 1 19 C170J1A F4 TIME MARK 1 20 S T S C17001A F5 429 OUT HS LS SELECT 21 C149J1 22 SEE C149J1 9 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GLOBAL NAVIGATION SATELLITE SENSOR GNSSU NO 2 GNSSU Function Connector Pin Connects To GEN PURP INPUT 2 C149J1 23 ARINC 429 41 GNSSU OUTPUT 2 24 ARINC 429
79. 73 RS 422 XMTR 1 ee 4 190J1A 50 L 190J1A 49 GND L GND RESERVED CLK EN RS 422 XMTR 2 H C190J1A 50 E190J1A 50 L C190J1A 49 L GND 190J1A 49 RESERVED CLK T SPARE SPARE PB GND OPEN BRG 0 VOR1 GND OPEN BRG 0 ADF1 GND OPEN BRG 0 FMS1 GND OPEN BRG lt gt VOR2 GND OPEN BRG lt gt ADF2 GND OPEN BRG lt gt FMS2 GND OPEN SPARE PB GND OPEN SPARE PB GND OPEN SPARE PB GND OPEN SPEED PUSH CHG GND OPEN 21 24 1103 11 C115J1 21 CRS PUSH DCT 1 GND OPEN 22 HDG TRK SEL 1 GND OPEN 23 H T PUSH SYNC 1 GND OPEN 24 DU 2 PBO GND OPEN 25 24 131J1 62 C115J1 25 DU 2 PB1 GND OPEN 26 24 131J1 60 C115J1 26 DU 4 2 PB2 GND OPEN 27 24 131J1 51 C115J1 27 DU 2 PB3 GND OPEN 115J1 28 24 131J1 50 C115J1 28 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 1 CONT DC 840 Function DU 2 DU 2 DU 2 SPARE 13 13 13 3 13 13 13 SPARE DU 4 DU 4 DU 4 ALT SEL KNOB DU 4 DU 4 na KNOB B1 PB4 GND OPEN PB5 GND OPEN PB GND OPEN PBO GND OPEN PB1 GND OPEN PB2 GND OPEN BO ls PB3 GND
80. 77 SEE 190J1A 6 BC RESERVED 78 SPARE FGC DISC 79 28V 0PEN m FIGURE 8 2 DME 2 A 429 RCVR 20 SPARE FWC DISC 82 28V 0PEN FMS DATA LOADER L 83 DTR OUT FMS RS 422 TX H 84 FGC RESERVED 85 SPARE FGC DISC IN 86 GND OPEN FGC AP DISCONNECT 87 FIGURE 8 11 GND OPEN TRIM DISCONNNECT OPEN GND 88 FIGURE 8 9 FGC RESERVED 190J1A 89 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pin Connects To I CROSS SERVOS OFF IN 190J1A 90 C190J1D 75 28V 0PEN 1 CROSS SERVO PWR OFF IN 91 C190J1D 76 28V 0PEN 1 CROSS CHANNEL SYNC IN 92 C190J1C 55 GND OPEN 1 CROSS PWR SENSE IN 93 C190J1C 44 28 V OPEN 1 DU 1 WRAPAROUND 94 13001 66 A 429 RCVR 9 C190J1A 94 E190J1A 94 1 L 95 130J1 79 G 190 1 95 E190J1A 95 96 SEE 190J1A 6 190J1A 47 FMS DATA LOADER H 97 12331 K CLOCK OUT C190J1A 97 E190J1A 97 FMS RS 422 TX L 123J1 J C190J1A 98 SPA 99 24 E H 09 24 A 429 XMTR 6 L AOI C esse seco GC PANEL BUTTON ARM 100 24 11J1 47 GND OPEN 101 SEE 190J1A 99 YD DISCONNECT OPEN GND 102 24 SIGNAL GROUND FGC RESERVED 103 TRIM RATE CMD OUT H
81. 996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 1 CONT DC 840 10 BP Function Connector Pin Connects To I SG TEST 1 GND OPEN 115J2 15 24 135J1 49 C115J2 15 190J1B 51 1 SG TEST 2 GND OPEN 16 24 C135J1 49 C115J2 16 C190J1B 51 I SG TEST 3 GND OPEN 17 E135J1 49 C115J2 17 E190J1B 51 ANNUN TEST GND OPEN 18 FIGURE 8 7 SPARE PB GND OPEN lt 19 SPARE PB GND OPEN 20 SPARE PB GND OPEN 21 DU 5 PBO RESERVED 22 GND OPEN DU 5 PB1 RESERVED 23 C130J1 60 GND OPEN C115J2 23 DU 5 PB2 24 C130J1 51 GND OPEN C115J2 24 DU 5 PB3 METRIC 25 C130J1 50 GND OPEN C115J2 25 DU 5 PB4 IN HPA 26 C130J1 47 GND OPEN C115J2 26 DU 5 PB5 RESERVED GND OPEN SPARE PB GND OPEN SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE 36 SPARE 115J2 37 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont CONTROL DISPLAY UNIT CDU NO 1 CD 810 Function Connector Pi Connects To SPARE 120J1 A 28 VDC POWER FIGURE 8 6 28 VDC POWER RETURN DC POWER GND LIGHTING COMMON L LIGHTING GND
82. 996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To RSB RESERVED C190J1B 58 SPARE CARD RESERVED 59 1 SPARE DIO DISC IN 60 GND OPEN 1 SPARE DIO DISC IN 61 GND OPEN 1 SPARE DIO DISC IN 62 GND OPEN 1 SPARE DIO DISC IN 63 GND OPEN 1 SPARE DIO DISC IN 64 GND OPEN SPARE DIO DISC IN 65 GND OPEN FGC RESERVED 66 IAC OVERHEAT GND OPEN 67 190J1D 48 C190J1D 48 E190J1D 48 PRI RADIO TUNE GND OPEN 68 SPARE DIO DISC IN 69 28V 0PEN RSB PRIMARY H 70 RSB PRIMARY L 71 SPARE FWC DISC IN 72 28V 0PEN RSB RESERVED 73 RSB RESERVED 74 AWP MASTER OUT GND OPEN 75 AURAL WARNING 76 AURAL WARNING 1 77 SPARE CARD RESERVED 78 SPARE CARD RESERVED 79 FMS INITIATE RECEIVE 80 GND OPEN FMS INITIATE TRANSFER 81 GND OPEN SPARE DIO DISC OUT 82 GND OPEN SPARE DIO DISC OUT C190J1B 83 GND OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Func
83. AC 1 OVERHEAT 43 190J1B 67 GND OPEN 190J1D 43 C190J1D 43 CHECK PFD ANNUN GND OPEN 44 FIGURE 8 15 SG 1 REV GND OPEN 45 135J1 40 CHASSIS GROUND E190J1D 46 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pin Connects To 0 SPARE DIO DISC OUT E190J1D 47 28V 0PEN 1 TAC 2 OVERHEAT GND OPEN 48 C190J1B 67 190J1D 48 C190J1D 48 SPARE DIO DISC OUT 49 28V 0PEN GC PANEL STROBE OUT L GC PANEL STROBE OUT H FGC RESERVED 52 SG 3 REV GND OPEN 53 E135J1 43 L 54 E128J1 D AT 3 SERVO TACH l 55 Wb E128J1 A SPARE FGC RVDT ANALOG IN AT 1 SERVO TACH 56 57 58 128J1 D 59 l l 128J1 A G ND L H L H L 60 C128J1 D AT 2 SERVO TACH l 61 C128J1 A ND GC PANEL L 62 BUTTON DATA H 63 AWP ENABLE 28V 0PEN 64 SPARE FGC DISC IN 65 28V 0PEN BC ID 1 GND OPEN E190J1D 66 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont
84. ARE SPARE PORT SEL 3 GND OPEN 135J1 45 PORT SEL 2 GND OPEN 135J1 42 PORT SEL 1 GND OPEN I D 3 GND OPEN I D 2 GND OPEN I D 1 GND OPEN RESERVED CHASSIS GND RESERVED RESERVED RESERVED RESERVED SOFTWARE ENABLE GND OPEN SOFTWARE ENABLE 100 GND OPEN 28 VDC POWER 101 28 VDC POWER 102 FIGURE 8 6 28 VDC POWER 103 28 VDC POWER RETURN 104 28 VDC POWER RETURN 105 28 VDC POWER RETURN 130J1 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 2 DU 870 Function Connector Pin Connects To 131J1 1 135J1 4 13 24 14 H BRIGHTNESS POT L W H L W t 2 WX DIMMING L 3 W 15 RESERVED 4 RESERVED 5 RESERVED RESERVED SPARE RESERVED RESERVED RESERVED RESERVED 13 SEE 131J1 1 14 SEE 131J1 1 15 SEE 131J1 2 RESERVED 16 RESERVED 17 RESERVED BUS 3 H 19 BUS 3 NO TERM l L 20 FIGURE 8 14 BEZEL KNOB B0 21 115J1 29 C115J1 29 DU PWR DN GND OPEN 22 0 5 VDC EDGE H 23 FIGURE 8 7 LIGHTING L 24 LIGHTING GND BEZEL KNOB B1 25 115J1 30 C115J1 30 REMOTE LT SENSOR H 26 REMOTE LT SENSOR L 131J1 27 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title pa
85. ARE SPARE RS 232 DATA RCVR RS 232 COMMON FIGURE 8 3 RS 232 DATA XMTR CO OOOOOOOGO r wow RESERVED C9J1 58 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document wwe wwe ww ww ww ww wwe na wwe n Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont MICRO AIR DATA COMPUTER MADC NO 2 cont AZ 840 Function Connector Pin Connects To ASCB NO 2 BACKUP H C9J1 59 ASCB NO 2 BACKUP L 62 ARINC 429 BUS 1 H 60 ARINC 429 BUS 1 L 61 62 63 L 64 65 FI ARINC 429 BUS 2 H ARINC 429 BUS 2 ASCB NO 1 PRI H ASCB NO 1 PRI L ARINC 429 BUS 3 H 66 ARINC 429 BUS 3 L 67 H ARINC 429 BUS 4 H 68 ARINC 429 BUS 4 L 69 FUNCTIONAL TEST GND OPEN 70 BARO STD SYNC GND OPEN 71 SSEC DISABLE 72 SPARE 73 BARO CORRECTION 74 BARO CORRECTION 75 SPARE 76 707 SPARE 78 SPARE C9J1 79 FIGURE 8 1 FIGURE 8 2 SEE C9J1 59 FIGURE 8 2 FIGURE 8 1 FIGURE 8 2 FIGURE 8 8 C130J1 46 FIGURE 8 8 C13001 21 C130J1 25 SEE C9J1 65 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTE
86. AWG from the mating connector outer shell to the airframe ground Connector pins designated Chassis Gnd will not be wired unless otherwise shown in this table Chassis Gnd pins which are designated to be connected should use a minimum length wire to airframe ground The purpose of this ground shall be to ensure that the LRU chassis is at the same potential as the local airframe to prevent electrical shock hazard Additionally this chassis to airframe ground will provide a low impedance path for rf energy from the LRU chassis external shield effectively shunting rf away from the internal circuitry THE CHASSIS GROUNDING TECHNIQUE SHOWN ABOVE SHALL BE ADHERED TO UNLESS OTHERWISE INDICATED IN THIS TABLE 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont All shielded wires shall have the shields grounded according to the scheme shown in paragraph 4 1 3 4 Shield ground references are shown only on critical functions ASCB shielding requirements are specified in paragraph 5 and DU WX bus shielding requirements are specified in paragraph 6 Twisted wires shall have at least two full turns per foot The shields can be daisy chained as long as the total length of the wires used to connect the shields including the wire that grounds the chain does n
87. B 104 FIGURE 8 6 DC POWER GND CH B 105 DC POWER GND DC POWER GND CH B 136J2A 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 Function Connector Pin Connects To R ITT AL 136J2B 1 R ITT CH 2 3 SPARE DC ANALOG 4 SPARE DC ANALOG 2 R N1 SPEED 7 R N1 SPEED 8 9 FUEL FLOW DRUM 10 FUEL FLOW COMMON 11 FUEL FLOW IMPELLER 12 FUEL HTR TEMP EXC 13 FUEL HTR TEMP EXC 14 FUEL HEATER TEMP 15 FUEL HEATER TEMP 16 17 OIL PRESSURE 18 OIL PRESSURE 19 20 TEMP EXC 21 22 TEMP 23 TEMP POT POT POT 35 136J2B 36 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 Function Connector Pin Connects To 136J2B 37 R N2 SPEED 38 R N2 SPEED 739 DEEC OUTPUT 40 ARINC 429 CH B 41 SPARE INPUT 42 ARINC 429 43 SPARE INPUT 44 ARINC 429 45 SPARE INPUT 46 ARINC 429 47 L AIR CONDITIONER ARINC 429 S T S FIGURE 8 2 SPARE OUTPUT ARINC 429 CH B RESERVED RESERVED
88. B RESET GND OPEN 89 DP2 RESET GND OPEN 90 RESERVED MASTER WARNING 91 HORN GND OPEN SPARE CARD RESERVED 92 SPARE CARD RESERVED 93 CONFIG MODULE 5V POWER 94 199J1 1 CONFIG MODULE RETURN 95 199J1 2 CONFIG MODULE DATA RX 96 199J1 3 SPARE DIO DISC IN 97 GND OPEN RESERVED WARNING RESET 98 GND OPEN RESERVED ON SIDE AWP 99 MASTER GND OPEN SPARE DIO DISC IN 100 28V 0PEN CROSS 28V YD CLUTCH IN 101 AT DISCONNECT GND OPEN 102 FIGURE 8 11 FGC RESET GND OPEN 103 FMS RS 232 COMMON 104 FMS RS 232 DATA RX 105 FIGURE 8 3 FMS RS 232 DATA TX 190J1B 106 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 0 0 0 0 Function Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 AIL SERVO DRIVE 190J1C 1 CCW DRUM ROTATION L 2 ELEV SERVO DRIVE 3 CCW DRUM ROTATION L 5 CROSS YD PWR SENSE OUT 28 V OPEN TRIM UP 28V GND SPARE H A 429 XMTR 5 L TRIM DN 28V GND 28V YD BRAKE OUT IOP RESERVED 28V AP CLUTCH OUT YD SERVO DRIVE L YD SERVO DRIVE H 13 26 GENERAL BUS 2 A 429 XMTR 3 14 190J1C 15 Connector Pi Pin 20 S T S L_GND 22 05 21 Connects To 12J1 A C190J1C 1 12J1 B C190J1C 2
89. C GND OPEN MADC VALID DISC GND OPEN ASCB NO 1 PRI H ASCB NO 1 PRI L IA IV IV IV IV TAS 27 28 29 Connector Pin 24 22 05 21 Connects To SIGNAL GND SIGNAL GND SIGNAL GND FIGURE 8 5 SIGNAL GND TO AIRCRAFT FIGURE 8 6 DC POWER GND OVERSPEED HORN FIGURE 8 1 Page 3 28 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont MICRO AIR DATA COMPUTER MADC NO 1 cont AZ 840 10 BP Function Connector Pin Connects To I TEMPERATURE PROBE H 9 1 31 24 5 S T S 500 OHM l l TEMPERATURE 1 TEMPERATURE PROBE 1 32 24 PROBE G SPARE 33 34 AOA POTENTIOMETER 35 ANGLE OF AOA POTENTIOMETER W 36 ATTACK AOA POTENTIOMETER L 37 POTENTIOMETER CALIBRATION ENABLE 38 GND OPEN SPARE 39 SPARE 40 ATC SELECT GND OPEN ATC Al ATC ATC ATC ATC ATC ATC ATC ATC ATC SPARE SPARE RS 232 DATA RCVR RS 232 COMMON FIGURE 8 3 RS 232 DATA XMTR RESERVED CO OOOOOOOGO r wow 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document wwe wwe ww ww ww ww wwe wwe PO IP Pe n
90. C130J1 101 C130J1 102 177W C130J1 103 C190J1D 6 C190J1D 7 125W C190J1D 8 C115J1 59TBD 136J2A 103 14W 136J2A 104 EST C190J1A 11 C190J1A 12 156W C190J1B 8 C190J1B 9 65W C120J1 B C120J1 v 55w C120J1 F C149J1 35 20W C131J1 101 C131J1 102 177W C131J1 103 AD 41484 R1 Page 3 221 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 0 5VDC 0 5VDC DIMMING 11J1 78 DIMMING C61J1 H Sone 61J1 H SUPPLY C115J1 76 115J1 76 COPILOT C120J1 J 120J1 J C130J1 23 130J1 23 C131J1 23 131J1 23 C135J1 53 132J1 23 C172J1 S 135J1 53 E135J1 53 172J1 S 28 VDC DAY 28 VDC DAY 14 VDC NIGHT 14 VDC NIGHT DIMMING DIMMING CONTROL 11J1 40 3 mA CONTROL 11J2 40 3 mA 61J1 K 75 mA C61J1 K 75 mA 120J1 w 600 mA COPILOT C120J1 w 600 mA 170J1C 10 450 mA C170J1C 10 450 mA 28 VDC DAY AIRCRAFT LAMP 14 VDC NIGHT TEST SWITCH DIMMING CONTROL E120J1 w 600 mA 11J1 51 E170J1C 10 450 mA 11J2 51 CENTER 115J2 18 C115J2 18 120J1 s C120J1 s 172J1 h C172J1 h E172J1 h E120J1 s AD 41497 R1 Lighting Power Dimming Lamp Test Figure 8 7 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 In
91. C190J1A 98 FIGURE 8 2 FIGURE 8 11 3 136 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 Function Connector Pin Connects To SPARE FMS DISC IN E190J1B 1 POWER RETURN AT POWER RETURN 3 DC POWER GND 28 VDC AIRCRAFT L 4 RAM BATTERY H zb FWC RESET GND OPEN 6 FGC RESERVED 7 28V AT SERVO POWER 8 28V AT SERVO POWER FIGURE 8 6 PITCH WHEEL 1 L 10 PITCH WHEEL 1 H 11 SPARE FMS DISC 12 GND OPEN ASCB NO 2 PRI 13 ASCB NO 2 PRI FIGURE 8 1 RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED RSB RESERVED 6 WX 2 RANGE UP OUT C61J1 L GND OPEN 190J1B 27 C190J1B 27 WX 2 RANGE DN OUT C61J1 N GND OPEN 190J1B 28 C190J1B 28 WX 1 RANGE UP OUT 6101 1 GND OPEN 190J1B 29 C190J1B 29 SEE E190J1B 13 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector
92. CB BUS 1 BACKUP L SEE FIGURE 8 1 CONNECTOR MS3122E22 558 OR EQUIVALENT l AC 1 di AC 1 DL IAC 1 BC IAC 3 FMS IAC 3 DL TX RX IAC 3 IOP COM TX RX IAC 3 BC COM ASCB NO 1 PRI ASCB NO 1 BU TEST CONN NO 1 LII TX MADC 2 RX COM IAC 2 FMS IAC 2 DL IAC 2 IOP IAC 2 BC ASCB NO 2 PRI ASCB NO 2 BU TEST CONN NO 2 C9J1 57 C9J1 55 C9J1 56 137J1B 104 137J1B 105 137J1B 106 137J2B 104 137J2B 105 137J2B 106 C149J1 2 C149J1 3 SIGNAL GND C170J1A H10 C170J1A H3 C170J1A H4 C170J1A H7 C190J1B 106 C190J1B 105 C190J1B 104 C190J1A 47 C190J1A 48 C190J1A 96 C190J1D 81 C190J1D 82 C190J1D 80 C190J1A 77 C190J1A 6 C190J1A 96 ASCB BUS 2 PRIMARY H ASCB BUS 2 PRIMARY L SEE FIGURE 8 1 ASCB BUS 2 BACKUP H ASCB BUS 2 BACKUP L SEE FIGURE 8 1 J CONNECTOR MS3122E22 55S OR EQUIVALENT RS 232 Test Connector Diagram Figure 8 3 22 05 21 AD 41494 R1 Page 3 217 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE MANUAL FALCON 900EX Honeywell Table 3 1 Interconnect Information cont LOGIC GND IRU ORIENT 1 IRU ORIENT 2 SDI 2 575 429 ADC SDI 1 a MSU 1 LOGIC GND a 170J1A LOGIC GND IRU ORIENT 1 IRU ORIENT 2 SDI 2 575 429 ADC SDI 1 LI MSU 3 LOGIC GND mn E170J1A
93. CLOCK H 24 er nee ae sss S C190J1D 97 2 PANEL CLOCK L 24 Re 5 C190J1D 96 ND GND G 12 PANEL STROBE H oA y S C190J1D 51 12 PANEL STROBE L 24 S C190J1D 50 GND G 12 BUTTON DATA H 24 S C190J1D 63 12 BUTTON DATA L day S s S C190J1D 62 GND SPARE SPARE GND OPEN SPARE SPARE SPARE SPARE 2 ADI BC GND OPEN SPARE GND OPEN 2 5 VDC POWER C190J1D 95 2 5 VDC POWER RETURN S C190J1D 94 2 28 VDC POWER FIGURE 8 6 2 28 VDC POWER RETURN DC POWER GND SPARE GND OPEN SPARE SPARE GND OPEN SPARE SPARE CHASSIS GND SPARE GND OPEN SPARE GND OPEN 1142 28 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GUIDANCE CONTROL PANEL GC cont GC 810 IO BP Function Connector Pin Connects To SPARE 1102 29 SPARE GND OPEN 30 SPARE SPARE SPARE GND OPEN SPARE GND OPEN SPARE GND OPEN SPARE GND OPEN 2 BC MODE 28V O0PEN SPARE SPARE DIMMING LEVEL DIMMING LEVEL ANN DRIVE PITCH WHEEL TACH H PITCH WHEEL TACH L 44 45 2 PB ARM IN GND OPEN 46 2 PB ARM OUT GND OPEN 47 C190J1A 100 RESERVED AP CLUTCH SPARE SPARE 0 2 LAMP TEST GND OPEN FIGURE 8 7 SPARE GND OPEN 2 11 L SEL
94. Connects To 5 VDC POWER 199J1 1 190J1B 94 5 VDC POWER RETURN 2 24 190J1B 95 DATA XMTR 199J1 3 190J1B 96 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 0 Function Connector Pin Connects To SIGNAL GROUND E190J1A 1 22 SIGNAL GND 28V ELEV TRIM CLUTCH OUT 2 TAC IDENT 2 GND OPEN 3 FGC RESERVED 4 ASCB NO 1 BU H ASCB NO 1 BU 1 FIGURE 8 1 BC RS 232 DATA RCVR BC RS 232 DATA XMTR FIGURE 8 3 BC DL RS 232 COMMON 28 VDC AT SERVO PWR RIN DC POWER GND 28 VDC AT SERVO PWR RTN DC POWER GND BC RESERVED 28 VDC AT SERVO POWER 28 VDC AT SERVO POWER FIGURE 8 6 SPARE H IOP RS 422 TX L DU 4 WRAPAROUND 0 C131J1 79 A 429 RCVR 12 190J1A 15 C190J1A 15 H C131J1 66 190J1A 16 C190J1A 16 TAG SYNC IN 1 17 190J1C 70 OPEN GND C19001A 17 TAG SYNC IN 2 18 190J1A 17 OPEN GND C190J1C 70 CDU SYNC IN 1 19 190J1C 69 OPEN GND C190J1A 19 ENERAL BU H A 429 XMTR 1 L E190J1A 21 FIGURE 8 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER
95. D RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 35 RESERVED 137J1A 36 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Function RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 Connector Pin Connects To 137J1A 37 38 ID 1 CH A GND OPEN 7 ID 2 CH A GND OPEN SIGNAL GND ID 3 CH A GND OPEN 137J1A 72 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 10 BP Function Connector Pin Connects To 137J1A 73 74 75 76 ASCB NO 2 PRI 77 DAU CHANNEL B S FIGURE 8 1 SEE 137J1A 77 ASCB NO 2 PRI H DAU CHANNEL A L S FIGURE 8 1 SIGNAL GROUND 1 CH A SIGNAL GND SIGNAL GROUND 2 CH A SIGNAL GND CHASSIS GROUND 101 102 28 VDC POWER CH A 103 28 VDC POWER CH A 104 FIGURE 8 6 DC POWER GND CH A 105 DC POWER GND DC POWER GND CH A 137J1A 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page
96. D OPEN BRG lt gt ADF2 GND OPEN BRG lt gt FMS2 GND OPEN SPARE PB GND OPEN SPARE PB GND OPEN SPARE PB GND OPEN SPEED PUSH CHG GND OPEN 21 24 1103 11 115J1 21 CRS PUSH DCT 1 GND OPEN 22 HDG TRK SEL 1 GND OPEN 23 H T PUSH SYNC 1 GND OPEN 24 DU 2 PBO GND OPEN 25 24 131J1 62 115J1 25 DU 2 PB1 GND OPEN 26 24 131J1 60 115J1 26 DU 4 2 PB2 GND OPEN 27 24 131J1 51 115J1 27 DU 2 PB3 GND OPEN C115J1 28 24 131J1 50 115J1 28 2 2 2 2 aaa 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 2 CONT DC 840 10 BP Function Connector Pin Connects To 1 BO 115 1 29 131J1 21 DU 2 KNOB 115J1 29 1 Bl 30 131J1 25 115J1 30 T DU 2 PB4 GND OPEN 31 131J1 47 115 1 31 1 DU 2 5 GND OPEN 32 131J1 46 115J1 32 1 SPARE GND OPEN 33 1 3 PBO GND OPEN 34 132J1 62 115J1 34 1 13 1 GND OPEN 35 132J1 60 115J1 35 1 3 2 GND OPEN 36 132J1 51 115J1 36 1 BO 37 132J1 21 3 KNOB 115J1 37 1 Bl 38 132J1 25 115J1 38 1 3 PB3 GND OPEN 39 132J1 50 115J1 39 1 3 PB4 G
97. E190J1A 62 LEFT EFIS PICTURE BUS H LEFT EFIS PICTURE BUS L FIGURE 8 14 CENTER EFIS PICTURE BUS i CENTER EFIS PICTURE BUS L j RIGHT EFIS PICTURE BUS H k RIGHT EFIS PICTURE BUS L s Suus FIGURE 8 14 190J1A 37 H LEFT EFIS CONTROL BUS C190J1A 37 E190J1A 37 190J1A 36 C190J1A 36 E190J1A 36 CONTROL BUS SHIELD p PICTURE BUS SHIELD q DADC DATA L r 429 RCVR H 5941 1 S FIGURE 8 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WEATHER RADAR RTA cont 0 10 BP Function Connector Pin Connects To 5901 5 SEE 59J1 k t SEE 59Jl r PARALLEL ALTITUDE BUS SPARE SPARE SPARE SPARE SPARE SPARE SPARE RESERVED 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WEATHER RADAR CONTROLLER NO WC 880 Function Connector Pi Connects To SERIAL CONTROL H 61 1 SERIAL CONTROL 1 B SPARE 28 VDC POWER D FIGURE 8 6 28 VDC POWER RETURN JE DC POWER GND CHASSIS GROUND F 0 28 VDC EDGE LIGHTING H G 0 5 VDC EDGE LIGHTING H H FIGURE 8 7 LIGHTING COMMON J LIGHTING GND 28 VDC ANNUN LIGHTING
98. ED CHARGER INHIBIT RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RS 232 DATA XMT RS 232 DATA RCV RS 232 COMMON RS 232 DIR RS 232 CTS RESERVED RESERVED MEM ACCESS WR E RESERVED RESERVED RESERVED RESERVED RESERVED SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Connector Pin 170J1A G1 RK 2 H 2 L G3 RK G9 R R NABLE H11 H12 H13 H14 170J1A H15 24 SEE 170J1A H3 22 05 21 Connects To C149J1 9 C149J1 22 BATT CHARGER INHIBIT INPUT FIGURE 8 3 FIGURE 8 3 Page 3 103 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III 10 BP Function Connector Pin Connects To RESERVED 170J1A J1 RESERVED J2 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED J8 SDI 3 GND OPEN 24 FIGURE 8 4 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED ASCB NO ASCB NO FIGURE 8 1 GND L_GND SEE 170J1A K3 RESERVED BITE WRITE INHIBIT ASCB 2 CLK H ASCB 2 CLK L RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 170J1A K15 SEE 170J1A K7 22 05 21 Sep
99. ED RESERVED RESERVED RESERVED J8 SDI 3 GND OPEN 24 FIGURE 8 4 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED ASCB NO 2 BU H ASCB NO 2 BU L FIGURE 8 1 GND L GND RESERVED SEE C170J1A K3 BITE WRITE INHIBIT ASCB 2 CLK H ASCB 2 CLK L RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 170 1 15 SEE C170J1A K7 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Function Connector Pin Connects To LOGIC GROUND C170J1B A1 FIGURE 8 4 IRU ORIENT 1 A2 FIGURE 8 4 IRU ORIENT 2 A3 FIGURE 8 4 RESERVED A4 RESERVED A5 RESERVED A6 501 2 GND OPEN A7 FIGURE 8 4 FMS PRI GEN BUS H A8 A 429 RCVR 1 L 9 REMOTE TEST GND OPEN A10 24 C172J1 W RESERVED A11 RESERVED A12 ISDU NDU NO 3 H A13 A 429 RCVR L A14 BATTERY FAIL ANNUN A15 24 17201 7 GND OPEN RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED C170J1B B15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell
100. ED RESERVED RESERVED RESERVED IRS DATA OUT 1 ARINC 429 XMTR RESERVED RESERVED RESERVED RESERVED RESERVED IRS DATA OUT 5 ARINC 429 XMTR RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED H13 IRS DATA OUT 6 H H14 ARINC 429 XMTR L 170J1B H15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III 10 BP Function Connector Pin Connects To RESERVED 170J1B J1 RESERVED J2 RESERVED J3 RESERVED J4 RESERVED J5 DADC 575 429 SEL J6 FIGURE 8 4 RESERVED J7 RESERVED J8 501 1 GND OPEN J9 24 FIGURE 8 4 SEC DADC DATA H J10 A 429 RCVR 5 L J11 RESERVED J12 RESERVED J13 RESERVED J14 ON BATTERY ANNUN J15 RESERVED K1 RESERVED K2 RESERVED K3 PRI DADC DATA K4 H A 429 RCVR 4 1 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED IRS DATA OUT 3 H ARINC 429 XMTR L RESERVED 1 RESERVED 170J1B K15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UN
101. EM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 Function Connector Pin Connects To SPARE CARD RESERVED 190J1A 22 SPARE CARD RESERVED 23 DU BUS TX 2 24 DU BUS TX 2 1 25 FIGURE 8 14 LRN 2 H 26 A 429 RCVR 15 L 27 FIGURE 8 2 DU 3 WRAPAROUND L 28 132J1 79 A 429 RCVR 11 C190J1A 28 E190J1A 28 29 132J1 66 G C190J1A 29 E190J1A 29 SPARE H 30 IOP RS 422 RX L 31 CDU SYNC IN 3 32 C190J1A 32 GND OPEN E190J1C 69 SPARE FMS DISC IN 33 GND OPEN SPARE FMS DISC IN 34 GND OPEN SPARE FWC DISC IN 35 GND OPEN WX CONTROL DATA 1 L 36 59J1 n IOP RS 422 RX C190J1A 36 E190J1A 36 H 37 59J1 m G C190J1A 37 E190J1A 37 SPARE CARD RESERVED 38 SPARE CARD RESERVED 39 MLS 2 H 40 A 429 RCVR 22 1 41 S T S FIGURE 8 2 DU 2 WRAPAROUND H 42 131J1 66 A 429 RCVR 10 C190J1A 42 E190J1A 42 L 190J1A 43 131J1 79 G C190J1A 43 E190J1A 43 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 1 Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 Function Connector Pin SPARE FWC DISC IN 190J01A 44 GND OPEN FMS DATA LOADER 45 DATA OUT FM
102. EN ATT ANNUNCIATOR GND OPEN D3 RESERVED D4 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 170J1B D15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Function Connector Pin Connects To NO COOLING AIR ANNUN 170J1B E1 24 172J1 Y GND OPEN ON DC ANNUNCIATOR E2 GND OPEN NAV RDY ANNUNCIATOR GND OPEN RESERVED IRS DATA OUT 2 H ARINC 429 XMTR L RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED MODE DISCRETE 1 172J1 e MODE DISCRETE 2 172J1 f ALIGN ANNUNCIATOR 172 1 GND OPEN RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED F13 IRS DATA OUT 4 14 24 S T ARINC 429 XMTR L 170J1B F15 24 S T FIGURE 8 2 GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Function Connector Pin Connects To RESERVED 170J1B G1 RESERVED G2 RESERV
103. ENNA 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WEATHER RADAR RTA P 870 Function Connector Pin Connects To 28 VDC POWER 59 1 28 VDC POWER FIGURE 8 6 TRANSMIT ON GND OPEN 115V 400 HZ STAB REF AIRSPEED REFERENCE AIRSPEED SIGNAL RETURN STAB REF COMMON 429 ADC GND OPEN SIGNAL GND PARALLEL ALTITUDE BUS GND OPEN ATTITUDE DATA A 429 RCVR FIGURE Ome ANALOG ROLL H ANALOG ROLL L 200 MV DEG REACT COMPENSATION OVERRIDE R SIGNAL GND GND OPEN AIRSPEED REF RETURN S WOW GND OPEN T FIGURE 8 5 REMOTE ON GND OPEN U 61 1 190J1B 45 C190J1B 45 E190J1B 45 AIRSPEED SIGNAL V 28 VDC POWER RETURN W 28 VDC POWER RETURN X DC POWER GND ANALOG AIRSPEED SELECT Y 26V 400HZ STAB REF 5901 7 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WEATHER RADAR RTA cont 0 Function Connector Pi Connects To ALTERNATE CONTROL 59 1 61 1 BUS L b S PRIMARY CONTROL BUS H 61 1 PRIMARY CONTROL BUS 1 S H 190J1A 61 RT EFIS CONTROL BUS C190J1A 61 E190J1A 61 L me 190J1A 62 G C190J1A 62
104. ESERVED WARNING RESET 98 GND OPEN RESERVED ON SIDE AWP 99 MASTER GND OPEN SPARE DIO DISC IN 100 28V 0PEN CROSS 28V YD CLUTCH IN 101 AT DISCONNECT GND OPEN 102 FIGURE 8 11 FGC RESET GND OPEN 103 FMS RS 232 COMMON 104 FMS RS 232 DATA RX 105 FIGURE 8 3 FMS RS 232 DATA TX E190J1B 106 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pin Connects To 0 AT 1 SERVO us E190J1C 1 20 S T S 128J1 B CCW DRUM 0 ROTATION CL A CAO er eee eee Sees ass 128J1 C GND L_GND 0 AT 2 SERVO DRIVE C128J1 B CCW DRUM 0 ROTATION E b 20 9c9 92 8 Sc C128J1 C GND L GND CROSS YD PWR SENSE OUT 28 V OPEN SEE E190J1C 3 TRIM UP 28V GND SPARE H A 429 XMTR 5 L TRIM DN 28V GND SEE E190J1C 7 28V AT CLUTCH 3 OUT E128J1 E G L GND 10 RESERVED 28V AT CLUTCH 1 2 OUT C128J1 E AT 3 SERVO DRIVE pn E128J1 C CCW DRUM ROTATION H 26 l l E128J1 B G GENERAL BUS 2 14 A 429 XMTR 3 15 FIGURE 8 2 LRN 3 16 429 RCVR 16 17 ST FIGURE 8 2 AFIS 18 A 429 RCVR 14 E190J1C 19 FIGURE 8 2 22 05 21 Sep 1 1996 Use or disclosure of information on thi
105. FD FOOT MAX MAX ATTENUATION 1 4db PER 100 FEET AT 1 MHZ ASCB CABLE CANNOT BE USED AD 30107 R1 WX DU Bus Interface Unterminated DU Figure 6 4 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont If termination resistors in the aircraft wiring are undesirable each DU has provisions for bus termination The high H or and low L or inputs are always used To terminate a bus at a given DU install a 6 inch maximum 24 AWG jumper wire between the L input and the TERM input as shown in Figure 6 5 and Figure 6 6 NOTE If a terminating DU is removed from the panel all remaining DUs utilizing that particular bus may fail to operate or may operate intermittently BUS INPUT TERM RECEIVER DU PICTURE AD 42184 DU Picture Bus Termination Provision Figure 6 5 50 MAX 23 MIN 23 WX 1MHZ PICTURE TERMINATED BUS DU UNTERMINATED UNTERMINATED DU DU NOTES 1 THE STUB SHEILDING CAN BE ELIMINATED BY CONSTRUCTING THE STUB AS SHOWN IN FIG 5 2 CABLE HONEYWELL PART NO 3718911 1 OR EQUIVALENT CHARACTERISTIC IMPEDANCE 70 7 OHMS CHARACTERISTIC CAPACITANCE 30 PFD FOOT MAX MAX ATTENUATION 1 4db PER 100 FEET AT 1 MHZ ASCB CABLE CAN
106. FMS DISC OUT 68 GND OPEN CDU SYNC OUT 69 190J1A 19 GND OPEN E190J1A 32 TAG SYNC OUT C190J1C 70 190J1A 17 GND OPEN E190J1A 18 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 Function Connector Pin Connects To FMS CDU DATA IN Hun C190J1C 71 24 S T S C120J1 N FMS RS 422 RX H 72 24 S C120J1 M SPARE CARD RESERVED 73 SPARE CARD RESERVED 74 SPARE CARD RESERVED 75 LIGHTNING SENSOR 76 L A 429 RCVR 7 FIGURE 8 2 SPARE A 429 XMTR 2 L SPARE CARD RESERVED SPARE CARD RESERVED SPARE FMS DISC OUT GND OPEN SPARE FMS DISC OUT GND OPEN SPARE FMS DISC OUT GND OPEN DU HDLC TX 1 H DU HDLC TX 1 L S FIGURE 8 14 SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SIGNAL GROUND SIGNAL GND SPARE CARD RESERVED SPARE f 10 RS 422 TX L FIGURE 8 2 96 LRN 1 A 429 RCVR 5 H 97 24 S t C19071C 98 24 S FIGURE 307E 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX
107. Fs CB7 3 of DMEs F900EX will always have 2 DMEs CB7 4 of DMEs CB7 5 of MLSs F900EX allows 0 1 or 2 MLSs CB7 6 of MLSs 7 7 CB8 0 UTC Clock Control 3 CB8 1 UTC Clock Control 2 CB8 2 UTC Clock Control 1 CB8 3 TAC Provides WX Control TAC never provides WX Control on F900EX CB8 4 of Rad Alts F900EX allows 1 or 2 rad alts CB8 5 Cat II ILS Enabled All combinations allowed CB8 6 Cat II MLS Enabled All combinations allowed CB8 7 1 CB9 0 LBS KGS Select All combinations allowed 11 combinations allowed 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISCRETE BYTE BIT GENERIC DESCRIPTION NOTES CB9 1 Slip Skid Enabled All combinations allowed CB9 2 ASCB Sensor Types Ignored 11 combinations allowed by FMS CB9 3 ACARS Installed ACARS is not allowed on the F900EX CB9 4 AT Installed in this IAC IAC 3 has an autothrottle IACs 1 and 2 do not CB9 5 SPARE CB9 6 SPARE CB9 7 1 CB10 0 Ctr Fuel Tank Temp Enabled 11 combinations allowed CB10 1 SPARE CB10 2 SPARE CB10 3 HGS Installed HGS is optional on F900EX CB10 4 SPARE CB10 5 SPARE CB10 6 SPARE CB10 7 1 CB11 0 SPARE CB11 1 GPWS Installed GPWS is optional on F900EX CB11 2 SPARE CB11 3 SPARE CB11 4 FD Operation Mode 2 Bezel selectable options not CB11 5 FD
108. GND OPEN C115J1 40 RESERVED BUS 2 TERM 49 DU 3 PB3 50 115J1 39 GND OPEN C115J1 39 DU 3 PB2 51 115J1 36 GND OPEN C115J1 36 BUS 1 TERM 52 REM LT SENSOR 53 REM LT SENSOR 132J1 54 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 3 cont DU 870 Function Connector Pin Connects To RESERVED 132J1 55 RESERVED 56 RESERVED 57 BUS 4 H BUS 4 NO TERM L 59 FIGURE 8 14 DU 3 PB1 60 115J1 35 GND OPEN C115J1 35 WX BUS 2 TERM 61 DU 3 PBO LEFT PB 62 115J1 34 GND OPEN C115J1 34 KNOB PB COMMON 63 SIGNAL GND WX BUS 1 TERM DU OVERTEMP GND OPEN 65 DU WRAPAROUND H 66 190J1A 29 A 429 XMTR C190J1A 29 E190J1A 29 L 79 5 5 190J1A 28 C190J1A 28 E190J1A 28 RESERVED 67 RESERVED WX BUS 3 en 69 132J1 70 WX BUS 3 NO TERM L L 70 132J1 69 RESERVED 71 RESERVED 72 RESERVED 73 WX BUS 2 132J1 75 WX BUS 2 NO TERM L 75 132J1 74 SPARE 76 WX BUS 1 ub 77 132J1 78 WX BUS 1 NO TERM 1 132J1 77 132J1 79 SEE 132J1 66 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Informatio
109. Honeywell Business and Commuter Aviation Systems Honeywell Inc Box 29000 Phoenix Arizona 85038 PRIMUS 2000 Integrated Avionics System Falcon 900 System Maintenance Manual Volume II System Interconnects Maintenance Practices Shipping Handling and Storage and Honeywell Support 22 05 21 TITLE PAGE T 1 PRINTED IN U S A PUB NO A15 1146 072 1 SEPTEMBER 1996 SYSTEM Honeywell FALCON 900EX PROPRIETARY NOTICE This document and the information disclosed herein are proprietary data of Honeywell Inc Neither this document nor the information contained herein shall be used reproduced or disclosed to others without the written authorization of Honeywell Inc except to the extent required for installation or maintenance of recipient s equipment NOTICE FREEDOM OF INFORMATION ACT 5 USC 552 AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY 18 USC 1905 This document is being furnished in confidence by Honeywell Inc The information disclosed herein falls within exemption b 4 of 5 USC 552 and the prohibitions of 18 USC 1905 S96 22 05 21 TITLE PAGE T 2 Copyright 1996 Honeywell Inc All Rights Reserved 1 SEPTEMBER 1996 Please cut along the dotted line Please cut along the dotted line Qe O99 Honeywell FOR HONEYWELL USE ONLY CUSTOMER RESPONSE CONTROL NO DATE RECEIVED To help us improve the quality of our publications Honeywell encourages reade
110. IAC NO 3 cont IC 800 Function Connector Pin Connects To SPARE CARD RESERVED E190J1A 22 SPARE CARD RESERVED 23 DU BUS TX 2 24 DU BUS TX 2 1 25 FIGURE 8 14 LRN 2 H 26 A 429 RCVR 15 L 27 FIGURE 8 2 DU 3 WRAPAROUND L 28 132J1 79 A 429 RCVR 11 190J1A 28 C190J1A 28 H 29 132J1 66 G 190J1A 29 C190J1A 29 SPARE 30 IOP RS 422 RX 31 CDU SYNC IN 2 32 190J1A 19 GND OPEN C190J1C 69 SPARE FMS DISC IN 433 GND OPEN SPARE FMS DISC IN 34 GND OPEN SPARE FWC DISC IN 35 GND OPEN WX CONTROL DATA 1 L 36 59J1 n IOP RS 422 RX 190J1A 36 C190J1A 36 H 37 59J1 m G 190J1A 37 C190J1A 37 SPARE CARD RESERVED 38 SPARE CARD RESERVED 39 MLS 2 H 40 A 429 RCVR 22 L 41 S T S FIGURE 8 2 DU 2 MRAPAROUND H 42 131J1 66 A 429 RCVR 10 190J1A 42 C190J1A 42 L E190J1A 43 131J1 79 G 190J1A 43 C190J1A 43 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 Function Connector Pin SPARE FWC DISC IN E190J1A 44 GND OPEN FMS DATA LOADER H 45 DATA OUT FMS RS 422 TX L 46 FMS DATA LOADER RS 232 TX FMS DATA LOADER RS 232 RX BC DL RS 232 COMMON DISPLAY CONTROL 1 L IOP RS 422 RX CH SPARE CARD RESERVED SPA
111. IC 800 Function Connector Pin Connects To SPARE FMS DISC OUT E190J1D 67 GND OPEN FMS HORN 68 24 FIGURE 8 15 GND OPEN SWITCHED LVDT RVDT EXCITATION RESERVED HDLC RX 1 H RESERVED HDLC RX 1 L FGC RESERVED FGC RESERVED CROSS SERVOS OFF 28V 0PEN 75 CROSS SERVOS PWR OFF 76 28V 0PEN AIL RVDT SURFACE POS 77 AIL RVDT SURFACE POS 78 BC ID 3 GND OPEN 79 SIGNAL GND IOP RS 232 COMMON 80 IOP RS 232 DATA XMTR 81 FIGURE 8 3 IOP RS 232 DATA RCVR 82 RESERVED HDLC RX 2 H 83 RESERVED HDLC RX 2 L 84 L RESERVED SBY ENG ENABLE 85 GND OPEN SPARE DIO DISC IN 86 GND OPEN SPARE DIO DISC IN 87 GND OPEN RESERVED FWC MEM ERASE 88 GND OPEN 28V AP CLUTCH IN E190J1D 89 20 Seager eer igi LG 28V 0PEN 13J1 G 190J1C 12 C190J1C 12 190J1D 89 C190J1D 89 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE MANUAL FALCON 900EX Honeywell Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function I RESERVED FWC Connector Pin Connects To E190J1D 90 DOWNLOAD INIT GND OPEN 1 28V YD BRAKE IN 28V 0PEN SPARE DIO DISC IN GND OPEN COPILOT STICKSHAKER 28V 0PEN GC PANEL POWER RETURN 5V GC PANEL POWER GC PANEL CLOCK GC PANEL CLOCK GC
112. IT NO 1 cont LASEREF III 0 BP Function Connector Pin Connects To 115 VAC INPUT 170J1C 1 24 VDC BATT INPUT 2 FIGURE 8 6 RESERVED 3 28 VDC ESSENTIAL 4 FIGURE 8 6 115 VAC RETURN 5 28 VDC MSU POWER OUTPUT 6 28 VDC PRIMARY POWER 7 FIGURE 8 6 28 VDC BATTERY POWER RTN 8 DC POWER GND ANNUNCIATOR POWER OUT 9 172J1 L ANNUNCIATOR POWER IN 10 FIGURE 8 7 CHASSIS GND 11 RESERVED 12 RESERVED 170J1C 13 TRAY FAN POWER RED 170J1C 7 TRAY FAN POWER GND BLK 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP 1 SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont TRS MODE SELECTION UNIT NO 1 MSU Function Connector Pin Connects To CHASSIS GND 172J1 A SPARE B SPARE SPARE SPARE SPARE SPARE SPARE SPARE ON BATT ANNUN PWR INPUT FIGURE 8 6 ANNUN PWR 170J1C 9 28 VDC IRU BLOWER M TRU BLOWER CONTROL 28V 0PEN FAULT ANNUN GND OPEN 170J1B D2 SPARE 0 5 VDC PANEL LIGHTING S 0 5 VDC PANEL LIGHTING L T LOGIC GND U TEST GND V TEST SW GND OPEN W NAV RDY ANNUN GND OPEN X NO AIR ANNUN GND OPEN Y BATT FAIL ANNUN GND OPEN Z ALIGN ANNUN GND OPEN a SPARE b SPARE SPARE d MODE SELECT 1 e 170J1B F1 MODE SELECT 2 172J1 f 170J1B F2 ON BATT ANNUN 172J1 g 170J1B J15 GND OPEN ANNUN TST GND OPEN h FIGURE 8 7 SPARE 17
113. LER DC NO 2 CONT DC 840 10 BP Function Connector Pin I SG TEST 1 GND OPEN C115J2 15 24 I SG TEST 2 GND OPEN 16 24 SG TEST 3 GND OPEN ANNUN TEST GND OPEN SPARE PB GND OPEN SPARE PB GND OPEN SPARE PB GND OPEN DU 5 PBO RESERVED GND OPEN DU 5 PB1 RESERVED GND OPEN DU 5 PB2 FPA GND OPEN DU 5 PB3 METRIC GND OPEN DU 5 PB4 IN HPA GND OPEN DU 5 PB5 RESERVED GND OPEN SPARE PB GND OPEN SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE 36 SPARE C115J2 37 22 05 21 Connects To 135J1 49 115J2 15 190J1B 51 C135J1 49 115J2 16 C190J1B 51 E135J1 49 115J2 17 E190J1B 51 FIGURE 8 7 C130J1 60 115J2 23 C130J1 51 115J2 24 C130J1 50 115J2 25 C130J1 47 115J2 26 Page 3 160 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont CONTROL DISPLAY UNIT CDU NO 2 CD 810 Function Connector Pi Connects To SPARE C120J1 A 28 VDC POWER FIGURE 8 6 28 VDC POWER RETURN DC POWER GND LIGHTING COMMON L LIGHTING GND SPARE 28 V ANN POWER H FIGURE 8 6 CHASSIS GND 28 V ANN POWER L DC POWER GND 0 5 V PANEL LIGHTING FIGURE 8 7 28 V PANEL LIGHTING SPARE NAV DATA OUT RS 422 XMTR C190J1C 72 C190J1C 71 C190J1C 59 C190J1C 58 C190J1C 52 C190J1C 51 C190J1C
114. LO 55 11 535 0513 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX 2 Ordering Information When placing an order Honeywell needs the following information e Part number with dash number of faulty unit Serial number of faulty unit Aircraft type serial number and registration number Aircraft owner Reported complaint with faulty unit e Service requested Exchange or Rental e Shipping address e f faulty unit is in warranty Type of warranty New or SPEX Date warranty started e If faulty unit is NOT in warranty provide billing address If faulty unit is covered under a maintenance contract Type of contract Contract 1 0 number Purchase order number NOTES 1 Units will ship same day or within 24 hours 2 Shipments within the U S will be shipped Next Day Air P M Delivery unless otherwise specified 3 Return Shipping Procedures a Shipping Container All components returned to Honeywell must be packed in the same or Honeywell approved equivalent container in which the component was received Components which are received in IMPROPER containers may be subject to DAMAGE charges NOTE Please ship the return unit to the support center indicated on the document provided Include completed multi page exchange amp rental
115. MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 4 DU 870 Function Connector Pin Connects To C131J1 1 C135J1 4 13 24 135 1 6 14 135 1 5 BRIGHTNESS POT L W H L W f 2 WX DIMMING L 3 15 RESERVED 4 RESERVED 5 RESERVED RESERVED SPARE RESERVED RESERVED RESERVED RESERVED 13 SEE C131J1 1 14 SEE C131J1 1 15 SEE C131J1 2 RESERVED 16 RESERVED 17 RESERVED BUS 3 H 19 BUS 3 NO TERM l L 20 FIGURE 8 14 BEZEL KNOB B0 21 115J1 45 C115J1 45 DU PWR DN GND OPEN 22 0 5 VDC EDGE H 23 FIGURE 8 7 LIGHTING L 24 LIGHTING GND BEZEL KNOB B1 25 115J1 46 11501 46 REMOTE LT SENSOR 26 REMOTE LT SENSOR L C131J1 27 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 4 cont DU 870 Function Connector Pin Connects To DLS H 131 1 28 24 S T S 130 1 29 DLS L 5 C130J1 42 GND ALS H Steen ee 5 C130J1 28 ALS L COA ka ance Hemos 5 C130J1 41 ND GND RESERVED RESERVED HDLC OUT RESERVED HDLC OUT BUS 3 TERM RESERVED BUS 2 FED BUS 2 NO TERM 1 DU VALID GND OPEN BUS 1 han BUS 1 NO TERM 1 REMOTE LT SENSOR GND SEE C
116. MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Function Connector Pin Connects To RESERVED C170J1B C1 RESERVED C2 RESERVED C3 RESERVED C4 FMS SEC GEN BUS H A 429 RCVR 2 L C6 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED FAULT ANNUNCIATOR C172J1 P GND OPEN ATT ANNUNCIATOR GND OPEN D3 RESERVED D4 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED C170J1B D15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Function Connector Pin Connects To NO COOLING AIR ANNUN C170J1B E1 24 C172J1 Y GND OPEN ON DC ANNUNCIATOR E2 GND OPEN NAV RDY ANNUNCIATOR C172J1 X GND OPEN RESERVED IRS DATA OUT 2 H ARINC 429 XMTR L RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED MODE DISCRETE 1 17201 MODE DISCRETE 2 C172J1 f ALIGN ANNUNCIATOR C172J1 a GND OPEN RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED F13 IRS DATA OUT 4 SEMA ea SI FIGURE 8 2 ARINC 429 XMTR L
117. NANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WEATHER RADAR CONTROLLER NO 2 WC 880 Function Connector Pi Connects To SERIAL CONTROL H C61J1 A SERIAL CONTROL L B SPARE 28 VDC POWER D FIGURE 8 6 28 VDC POWER RETURN JE DC POWER GND CHASSIS GROUND F 0 28 VDC EDGE LIGHTING H G 0 5 VDC EDGE LIGHTING H H FIGURE 8 7 LIGHTING COMMON J LIGHTING GND 28 VDC ANNUN LIGHTING DIM K FIGURE 8 7 RANGE UP 190J1B 27 C190J1B 27 E190J1B 27 SHIELD GND RANGE DN 190J1B 28 C190J1B 28 E190J1B 28 FORCED SBY NO 1 GND OPEN P FIGURE 8 5 REMOTE ON GND OPEN R 5901 0 61J1 R 190J1B 45 C190J1B 45 E190J1B 45 FORCED SBY NO 2 GND OPEN S OFF IN OFF OUT C61J1 U 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 2 DC 840 Function Connector Pin Connects To 28 V DC POWER RETURN C115J1 1 22 DC POWER GND SIGNAL GROUND 2 SIGNAL GND CHASSIS GROUND 73 RS 422 XMTR 1 ee 4 C190J1C 38 L C190J1C 39 GND L GND RESERVED CLK EN H 190J1C 38 RS 422 XMTR 2 E190J1C 38 L S 190J1C 39 L GND E190J1C 39 RESERVED CLK T SPARE SPARE PB GND OPEN BRG 0 VOR1 GND OPEN BRG 0 ADF1 GND OPEN BRG 0 FMS1 GND OPEN BRG lt gt VOR2 GN
118. ND CONNECTION TO ASCB SHIELD ASCB Stub Construction Figure 5 2 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 6 6 0 1 SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT BUS INTERFACE REQUIREMENTS IAC Display Unit Bus Interface The IAC DU buses provide PFD MFD and EID data from the IACs to the DUs The following paragraphs define the electrical interface requirements for the IAC DU interconnect The IAC DU transmission lines must satisfy the same electrical characteristics as ASCB cable but not the same environmental characteristics The electrical characteristic requirements are a characteristic impedance of 125 5 ohms and a characteristic capacitance of 12 2 picofarads foot Raychem 2524E0114 with thermorad jacket cable Filotex Part No 69654 cable or other cable that satisfies the stated electrical requirements can be used To allow dispatch without all DUs installed the preferred method of IAC DU interconnect is to provide the bus termination resistors in the aircraft wiring This allows any display or displays to be removed and not affect operation of the remaining displays This method is shown in Figure 6 1 and Figure 8 14 SG 1MHZ BUS UNTERMINATED DU DU 1 THE STUB SHEILDING CAN BE ELIMINATED BY CONSTRUCTING THE STUB AS SHOWN IN FIG 5 2 CABLE
119. ND C190J1C 10 SPARE CHASSIS GND SPARE BRAKE DC POWER GND SPARE SPARE SPARE LVDT OUTPUT bs 190J1D 54 l C190J1D 54 LVDT OUTPUT 190J1D 55 SPARE C190J1D 55 SEE 14J1 C SPARE SPARE LVDT EXCITATION s 190J1D 70 C190J1D 70 LVDT EXCITATION C 190J1D 69 G L GND C190J1D 69 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont RADIO ALTIMETER RT 300 10 BP Function Connector Pin Connects To SPARE 20 1 TEST INHIBIT 2 GND OPEN SPARE TEST INHIBIT 1 GND OPEN OUTPUT TEST TRACK INVALID GND OPEN SPARE SPARE SPARE SPARE TRIP NO 4 500 FT 15 VDC COMMON 20 2 ALT TRIP COMMON TRIP NO 3 50 FT SPARE TEST GND OPEN TRIP NO 1 1200 FT TRIP NO 2 250 FT LT OUTPUT E OUTPUT COMMON FIGURE 8 13 AUX OUTPUT OUTPUT COMMON GPWS GND RAD ALT VALID 28 V OPEN FIGURE 8 13 15 VDC Z 15 VDC 28 VDC POWER RETURN 22 DC POWER GND 28 VDC POWER FIGURE 8 6 wwe FIGURE 8 13 1 C UU gt OOOD NA wwe LNT TS 2 2 2 TRANSMIT TRANSMIT SHIELD ANTENNA RECEIVE RECEIVE SHIELD ANT
120. ND OPEN 40 132J1 47 115J1 40 1 3 PB5 GND OPEN 41 132J1 46 115J1 41 I SPARE PB GND OPEN 42 1 DU 4 PBO GND OPEN 43 C131J1 62 115J1 43 D DU 4 PB1 GND OPEN 44 C131J1 60 115J1 44 I BO 45 C131J1 21 DU 4 KNOB 115J1 45 1 Bl 46 C131J1 25 115J1 46 1 BO 47 1103 5 ALT SEL KNOB 115J1 47 I Bl 48 1143 6 115J1 48 1 DU 4 2 GND OPEN 49 C131J1 51 115J1 49 1 DU 4 PB3 GND OPEN C115J1 50 C131J1 50 115J1 50 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE MANUAL FALCON 900EX Honeywell Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 2 CONT DC 840 10 BP Function Connector Pin 1 DU 4 GND OPEN C115J1 51 24 1 DU 4 5 GND OPEN 52 1 SPARE PB GND OPEN 53 1 IRS REV 1 GND OPEN 54 1 ADC REV 1 GND OPEN 55 1 IRS REV 2 GND OPEN 56 1 ADC REV 2 GND OPEN 57 1 DAU 1 REV GND OPEN 58 Connects To C131J1 47 115J1 51 C131J1 46 115J1 52 135J1 52 115J1 54 135J1 51 115J1 55 C135J1 52 115J1 56 C135J1 51 115J1 57 E135J1 51 115J1 58 1 1 28 DC POWER DAU 2 REV GND OPEN DH MDA GND OPEN SPARE SPARE SPARE SPARE MIN SEL KNOB HDG TRK KNOB CRS KNOB SPARE KNOB SPARE KNOB 4 C115J1 75 22 05 21 FIGURE 8 6 E135J1 52 115J1 60 1103 4 115 1 61 1103
121. NEL A L S FIGURE 8 1 SIGNAL GROUND 1 CH B 99 SIGNAL GND SIGNAL GROUND 2 CH B 100 SIGNAL GND CHASSIS GROUND 101 102 28 VDC POWER CH B 103 28 VDC POWER CH B 104 FIGURE 8 6 DC POWER GND CH B 105 DC POWER GND DC POWER GND CH B 137J2A 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MAINTE FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 Function SPARE THERMOCOUPLE SPARE SPARE SPARE SPARE SPARE SPARE SPARE DC ANALOG DC ANALOG FUEL FLOW FUEL FLOW FUEL FLOW C FUEL TEMP EXC C FUEL TEMP EXC C FUEL TEMP C FUEL TEMP SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE SPARE DC ANALOG DC ANALOG RTD EXC RTD EXC RTD RTD POT POT POT Connector Pin Connects To AL 137J2B 1 CH 2 3 4 5 6 8 9 DRUM 10 COMMON 11 IMPELLER 12 H 13 14 15 16 17 18 19 20 21 22 23 GND L_GND S GND L GND 5 137J2B 36 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 Function Connector
122. NOT BE USED AD 30105 R1 WX DU Bus Interface Terminated DU Figure 6 6 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont The maximum cable length for a WX DU picture bus from the WX to its termination is 50 feet There shall be a minimum of 23 inches of cable between adjacent stubs ref Figure 6 4 and 6 6 The preferred method of constructing a DU stub connection is the same as for the ASCB stub ref Figure 5 2 Using this method the unshielded stub length can be up to 6 inches Butt splices with solder rings will be utilized for all stub interconnections ref Figure 5 2 The bus shield connections at each stub shall be accomplished with a butt splice which will provide a maximum shield to shield connection of 0 3 inches If a stub shield is used connect the stub shield to the bus shield with a butt splice of minimum length less than 2 inches 20 AWG wire All exposed wires at the splice and wires used to connect shields at the splice shall be covered with an overbraid material The overbraid material shall then be tied to the shield or airframe ground The bus shields shall be grounded to the airframe ground at each LRU connector with a minimum length 20 AWG wire Refer to paragraph 4 1 3 4 for proper shield grounding points and overbraid
123. O 1 cont IC 800 IO BP Function Connector Pin Connects To RSB RESERVED 190J1B 58 SPARE CARD RESERVED 59 1 SPARE DIO DISC IN 60 GND OPEN 1 SPARE DIO DISC IN 61 GND OPEN 1 SPARE DIO DISC IN 62 GND OPEN 1 SPARE DIO DISC IN 63 GND OPEN 1 SPARE DIO DISC IN 64 GND OPEN SPARE DIO DISC IN 65 GND OPEN FGC RESERVED 66 IAC OVERHEAT GND OPEN 67 190J1D 43 C190J1D 43 E190J1D 43 PRI RADIO TUNE GND OPEN 68 SPARE DIO DISC IN 69 28V 0PEN RSB PRIMARY H 70 RSB PRIMARY L 71 SPARE FWC DISC IN 72 28V 0PEN RSB RESERVED 73 RSB RESERVED 74 AWP MASTER OUT GND OPEN 75 AURAL WARNING 76 AURAL WARNING 1 77 SPARE CARD RESERVED 78 SPARE CARD RESERVED 79 FMS INITIATE RECEIVE 80 GND OPEN FMS INITIATE TRANSFER 81 GND OPEN SPARE DIO DISC OUT 82 GND OPEN SPARE DIO DISC OUT 190J1B 83 GND OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pin Connects To I SPARE DIO DISC IN 190J1B 84 GND OPEN 1 SPARE DIO DISC IN 85 GND OPEN 1 RESERVED CROSS SIDE 86 AWP MASTER GND OPEN 1 PILOT STICKSHAKER 87 FIGURE 8 12 28V 0PEN SPARE DIO DISC IN 88 28V 0PEN RS
124. ON CRITICAL ENSURE THAT PART NUMBER MARKED ON ACTUATOR IDENTIFICATION PLATE IS 7002800 901 CAUTION DO NOT APPLY TORQUE BETWEEN OUTPUT ROD AND HOUSING DURING INSTALLATION EVIDENCE OF TORQUE DAMAGE IS MISALIGNMENT GREATER THAN 5 DEGREES OF THE OUTPUT ROD KEY SLOT AND INDEX MARK a Before assembling actuator ensure actuator is set to mid stroke Length of actuator at mid stroke is 9 020 to 9 120 inches as shown in Figure 4 6 If not at mid stroke center actuator NOTES 1 To center actuator brake must be released by applying 28 volts dc to pin E with pin F connected to ground 2 Refer to Figure 4 6 for parts location of attaching hardware in the following steps 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX THREAD ACTUATOR LOCKING WASHER ENGAGEMENT 0 70 in 17 78 mm FORK END LOCKING NUT X BEARING ASSEMBLY m IN 1222222 THREAD ENGAGEMENT 0 56 14 22 mm 2 WASHER 71 9 020 to 9 120 in 229 10 to 231 65 mm 11 78 in 299 21 mm AD 47101 Figure 4 6 SM 725 Actuator Complete Assembly b Assemble locking nut and washer to housing end of actuator INSTALLATION CRITICAL THREAD ENGAGEMENT WITH FORK END ASSEMBLY MUST BE 0 70 IN 17 78 MM MINIMUM c Thread fork end assembly to actua
125. OP RESERVED 28V AP CLUTCH OUT 13 26 YD SERVO DRIVE L YD SERVO DRIVE H 15 16 C190J1C 17 GENERAL BUS 2 A 429 XMTR 3 LRN 3 429 RCVR 16 Connector Pi Pin 20 S T S L_GND 22 05 21 Connects To 12J1 A 190J1C 1 12J1 B 190J1C 2 13 1 190J1C 3 13J1 B 190J1C 5 190J1A 106 FIGURE 8 9 FIGURE 8 9 14J1 E 190J1C 10 190J1D 91 C190J1D 91 E190J1D 91 12J1 G 13J1 G 190J1C 12 190J1D 89 C190J1D 89 E190J1D 89 14J1 B 190J1C 13 14J1 A 190J1C 26 FIGURE 8 2 FIGURE 8 2 3 197 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 Function Connector Pin Connects To AFIS C19001C 18 A 429 RCVR 14 CL 1 DU 5 WRAPAROUND H 20 A 429 RCVR 13 L 21 SPARE FGC DISC IN 22 GND OPEN SPARE FGC DISC IN 23 GND OPEN 24 SPARE A 429 RCVR 18 25 26 SPARE CARD RESERVED 27 qn 28 L 29 MLS 1 A 429 RCVR 4 EICAS LEFT SEL 30 GND OPEN PFD 1 OFF GND OPEN 31 AURAL WARNING OUT 32 AURAL WARNING OUT B L 33 RSB RESERVED 34 RSB RESERVED 35 RSB SECONDARY H 36 RSB SECONDARY L 37 DISPLAY CONTROL 2 38 IOP RS 422 RX
126. OPEN PB4 GND OPEN PB5 GND OPEN PB GND OPEN PBO GND OPEN PB1 GND OPEN BO ln BO 2 GND OPEN PB3 GND OPEN KNOB KNOB Connector Pin 115J1 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 115J1 50 Connects To 131J1 21 C115J1 29 131J1 25 C115J1 30 131J1 47 C115J1 31 131J1 46 C115J1 32 132J1 62 C115J1 34 132J1 60 C115J1 35 132J1 51 C115J1 36 132J1 21 C115J1 37 132J1 25 C115J1 38 132J1 50 C115J1 39 132J1 47 C115J1 40 132J1 46 C115J1 41 C131J1 62 C115J1 43 C131J1 60 C115J1 44 C131J1 21 C115J1 45 C131J1 25 C115J1 46 1103 5 C115J1 47 1103 6 C115J1 48 C131J1 51 C115J1 49 C131J1 50 C115J1 50 Page 3 48 Sep 1 1996 22 05 21 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY CONTROLLER DC NO 1 CONT DC 840 10 BP Function Connector Pin Connects To 1 DU 4 4 GND OPEN 115J1 51 24 C131J1 47 C115J1 51 1 DU 4 5 GND OPEN 52 C131J1 46 C115J1 52 I SPARE PB GND OPEN 53 1 IRS REV 1 GND OPEN 54 135J1 52 C115J1 54 D ADC REV 1 GND OPEN 55 135J1 51 C115J1 55 1 IRS REV 2 GND OPEN 56 C135J1 52 C115J1 56 1 ADC REV 2 GND OPEN 57 C135J1 51 C115J1 57 1 DAU 1 REV GND OPEN
127. Operation Mode 1 allowed on F900EX CB11 6 SPARE CB11 7 1 CB12 0 AIRCRAFT F900EX ID 1 6 010100 CB12 1 AIRCRAFT CB12 2 AIRCRAFT CB12 3 AIRCRAFT CB12 4 AIRCRAFT CB12 5 AIRCRAFT CB12 6 SPARE CB12 7 1 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont The following pages will define the discretes for the configuration module Jumper Installed Logic 0 Jumper Removed Logic 1 of ASCB Attitude Sensors Installed 2 Discretes of ASCB Attitude Sensors Installed Config 2 Config 1 Dual ASCB Att Sensors 0 Triplex ASCB Att Sensors 0 Quad ASCB Att Sensors 1 Invalid 1 1 of Air Data s Installed 2 Discretes of Air Data s Installed Config 4 Config 3 Dual Air Data s 0 Triplex Air Data s 0 Quad Air Data s 1 Invalid 1 of EFIS FWC s Installed 2 Discretes of EFIS FWC s Installed Config 46 Config 5 Dual EFIS FWC s 0 Triplex EFIS FWC s 0 Quad EFIS FWC s 1 Invalid 1 Lightning Sensor Installed 1 Discrete Lightning Sensor Installed Config 7 Lightning Sensor Not Installed 0 Lightning Sensor Installed 1 AFCS Not Installed in this IAC AFCS Not Installed in this IAC Config 8 AFCS Installed in this IAC 0 AFCS Not Installed in this IAC 1 22 05 21 Sep 1 1996 Use or disclosure of information on
128. PANEL ANNUN DATA GC PANEL ANNUN DATA TRIM ARM UP OUT 28V 0PEN FMS RESET GND OPEN SPARE DIO DISC IN GND OPEN WEIGHT ON WHEELS GND OPEN ASCB NO 1 PRI ASCB NO 1 PRI L TRIM ARM DN OUT 28V 0PEN 14 1 190J1C 10 C190J1C 10 190J1D 91 C190J1D 91 91 22 S S G L GND 92 93 94 95 96 97 98 99 100 101 102 103 24 FIGURE 8 5 mee FIGURE 8 1 105 E190J1D 106 SEE E190J1D 104 Page 3 150 Sep 1 1996 22 05 21 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont TAC INSTALLATION MODULE NO 3 IM 803 Function Connector Pin Connects To 5 VDC POWER E199J1 1 E190J1B 94 5 VDC POWER RETURN 2 24 E190J1B 95 DATA XMTR E199J1 3 E190J1B 96 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont MICRO AIR DATA COMPUTER MADC NO 2 0 Function Connector Pin Connects To UNIT IDO GND OPEN C9J1 1 24 SIGNAL GND UNIT ID1 GND OPEN 2 UNIT ID2 GND OPEN 3 UNIT ID3 GND OPEN SIGNAL GND UNIT ID4 GND OPEN 5 UNIT ID5 GND OPEN UNIT ID6 GND OPEN SDI 1 GND OPEN SDI 2 GND OPEN
129. PEN RESERVED FWC MEM ERASE 88 GND OPEN 28V AP CLUTCH IN 190J1D 89 S 12J1 G 28V 0PEN L GND 13J1 G 190J1C 12 C190J1C 12 C190J1D 89 E190J1D 89 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pin Connects To I RESERVED FWC 190J1D 90 DOWNLOAD INIT GND OPEN 1 28V YD BRAKE IN 91 14J1 E 28V 0PEN G 190J1C 10 C190J1C 10 C190J1D 91 E190J1D 91 SPARE DIO DISC IN GND OPEN COPILOT STICKSHAKER FIGURE 8 12 28V 0PEN GC PANEL POWER RETURN 11J1 18 5V GC PANEL POWER 1101 17 GC PANEL CLOCK 11J1 4 GC PANEL CLOCK S T S 11 1 3 GC PANEL ANNUN DATA 1 1141 2 GC PANEL ANNUN DATA S T S 11J1 1 TRIM ARM UP OUT FIGURE 28V 0PEN FMS RESET GND OPEN SPARE DIO DISC IN GND OPEN WEIGHT ON WHEELS FIGURE GND OPEN ASCB NO 1 PRI ASCB NO 1 PRI L 5 FIGURE TRIM ARM DN OUT FIGURE 28V 0PEN 190J1D 106 SEE 190J1D 104 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont TAC INSTALLATION MODULE NO 1 IM 803 Function Connector Pin
130. PEN SPARE FMS DISC OUT GND OPEN SPARE FMS DISC OUT GND OPEN DU HDLC TX 1 H DU HDLC TX 1 L S FIGURE 8 14 SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SIGNAL GROUND SIGNAL GND SPARE CARD RESERVED SPARE t 10 RS 422 TX L 96 LRN 1 H 97 24 S T A 429 RCVR 5 E190J1C 98 24 S T FIGURE 8 2 GND LGND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COM GND L GND PUTER NO 3 cont IC 800 IO BP Function Connector Pin Connects To E190J1C 99 100 1 A 429 RCVR 8 FIGURE 8 2 DME 1 101 A 429 RCVR 2 102 FrouRE 8 2 ADF 1 103 A 429 RCVR 1 FIGURE 8 2 SPARE CARD RESERVED 105 SIGNAL GROUND E190J1C 106 SIGNAL GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pi Connects To I RESERVED LX ON E190J1D 1 OPEN GND 1 TAC 3 OVERHEAT GND OPEN 2 190J1D 2 C190J1D 2 E190J1B 67 PO
131. Pin Connects To 0 WX 1 RANGE DN OUT E190J1B 30 24 GND OPEN 190J1B 30 C190J1B 30 0 SPARE DIO DISC OUT 31 28V 0PEN 0 SPARE DIO DISC OUT 28V 0PEN RSB RESERVED AP OFF HORN GND OPEN RSB RESERVED DP1 RESET GND OPEN SPARE DIO DISC OUT GND OPEN SPARE DIO DISC IN GND OPEN SPARE DIO DISC OUT GND OPEN RSB RESERVED CAUTION RESET GND OPEN FIGURE 8 11 CDU VALID GND OPEN E120J1 i SEC RADIO TUNE GND OPEN ALT ALERT HORN GND OPEN FIGURE 8 15 WX ON GND OPEN 5901 0 61J1 R 61 1 190J1B 45 C190J1B 45 WARNING ANNUN GND OPEN DU 2 REV GND OPEN RAD ALT TEST GND OPEN 4 FIGURE 8 13 EICAS RIGHT SEL GND OPEN E135J1 10 DAUI REV FIGURE 8 2 GND OPEN SG TEST IN E135J1 49 GND OPEN 115J2 17 C115J2 17 SPARE DIO DISC IN GND OPEN RSB RESERVED BC RESERVED BC RESERVED BC RESERVED 6 BC IDENT 2 E190J1B 57 GND OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pin Connects To RSB RESERVED E190J1B 58 SPARE CARD RESERVED 59 1 SPARE DIO DISC IN 60 GND OPEN 1 SPARE DIO DISC IN 61 GND OPEN 1 SPARE DIO DISC IN 62 GND OPEN 1 SPARE DIO DISC IN 63 GND OPEN 1 SPARE DIO
132. Pin Connects To 137J2B 37 SPARE TACH 38 SPARE TACH 39 DEEC OUTPUT Pe ARINC 429 CH B FIGURE 8 2 L_GND SPARE INPUT ARINC 429 SPARE INPUT ARINC 429 SPARE INPUT ARINC 429 R AIR CONDITIONER ere ARINC 429 PN FIGURE 8 2 L_GND SPARE OUTPUT ARINC 429 CH B RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 69 RESERVED 137J2B 70 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 10 BP Function Connector Pin Connects To 137J2B 71 72 SPARE DC ANALOG SPARE DC ANALOG ASCB NO 1 BU DAU CHANNEL A FIGURE 8 1 GND L_GND 95 96 SEE 137J2B 94 97 RESERVED 98 RESERVED 99 RESERVED 100 RESERVED 101 102 103 RS 232 DATA CH B XMTR 104 24 S RS 232 DATA CH B RCVR 105 24 S FIGURE 8 3 RS 232 CH B COMMON _ 137J2B 106 24 AS ND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GLOBAL NAVIGATION SATELLITE SENSOR GNSSU NO 1 GNSSU 10 BP Fun
133. RE CARD RESERVED V L 2 A 429 RCVR 21 L IOP RS 422 RX IAC IDENT 1 GND OPEN SPARE en H L SPARE in L E IOP RS 422 TX L IDENT 0 GND OPEN WX CONTROL DATA 2 H IOP RS 422 RX 1 FMS DATA LOADER 63 DATA IN FMS RS 422 RX L E190J1A 64 Connects To 190J1A 45 C190J1A 45 123J1 G 190J1A 46 C190J1A 46 FIGURE 8 3 115J1 8 C190J1A 49 115J1 7 C190J1A 50 FIGURE 8 2 SIGNAL GND 59J1 e 190J1A 61 C190J1A 61 59J1 f 190J1A 62 190 1 62 123J1 T 190J1A 63 C190J1A 63 123J1 S 190J1A 64 C190J1A 64 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 0 BP Function Connector Pin Connects To FMS DATA LOADER H E190J1A 65 CTS IN FMS RS 422 RX L 66 ADF 2 un 67 A 429 RCVR 19 1 68 FIGURE 8 2 GND L GND HEAD UP DISPLAY H 69 24 A 429 RCVR 8 ee 70 24 FIGURE 8 2 GND L GND FGC RESERVED 71 MANUAL TRIM SELECT 72 SPARE FWC DISC IN 73 GND OPEN SPARE FWC DISC IN 74 GND OPEN SPARE FWC DISC IN 75 GND OPEN SPARE FWC DISC IN 76 GND OPEN 77 SEE E190J1A 6 BC RESERVED 78 SPARE FGC DISC 79 28V 0PEN a FIGURE 8 2 DME 2 A 4
134. RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED 69 RESERVED 136J2B 70 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 10 BP Function Connector Pin Connects To 136J2B 71 72 SPARE DC ANALOG SPARE DC ANALOG ASCB NO 2 BU DAU CHANNEL A FIGURE 8 1 GND L_GND 95 96 SEE 136J2B 94 97 RESERVED 98 RESERVED 99 RESERVED 100 RESERVED 101 102 103 RS 232 DATA CH B XMTR 104 24 S RS 232 DATA CH B RCVR 105 24 5 FIGURE 8 3 RS 232 CH B COMMON 13602 106 24 Am ND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 DA 800 10 BP Function Connector Pin Connects To RESERVED 137J1A 1 RESERVED 2 RESERVED 3 RESERVED 4 RESERVED 5 RESERVED 6 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVE
135. RS 422 RX L 66 ADF 2 un 67 A 429 RCVR 19 1 68 FIGURE 8 2 GND L GND HEAD UP DISPLAY H 69 24 A 429 RCVR 8 ee 70 24 FIGURE 8 2 GND L GND FGC RESERVED 71 SPARE FGC DISC 72 GND OPEN SPARE FWC DISC 73 GND OPEN SPARE FWC DISC 74 GND OPEN SPARE FWC DISC 75 GND OPEN SPARE FWC DISC 76 GND OPEN 77 SEE 190 1 6 BC RESERVED 78 SPARE FGC DISC 79 28V 0PEN a FIGURE 8 2 DME 2 A 429 RCVR 20 SPARE FWC DISC 82 28V 0PEN FMS DATA LOADER L 83 DTR OUT 84 FMS RS 422 TX H 85 SPARE FGC DISC IN 86 GND OPEN FGC AP DISCONNECT 87 FIGURE 8 11 GND OPEN TRIM DISCONNNECT OPEN GND 88 FIGURE 8 9 FGC RESERVED C190J1A 89 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To I CROSS SERVOS OFF IN C190J1A 90 190J1D 75 28V 0PEN 1 CROSS SERVO PWR OFF IN 91 190J1D 76 28V 0PEN 1 CROSS CHANNEL SYNC IN 92 190J1C 55 GND OPEN 1 CROSS AP PWR 93 190J1C 44 SENSE IN 28 V OPEN 1 DU 1 WRAPAROUND H 94 130J1 66 A 429 RCVR 9 190J1A 94 E190J1A 94 1 L 95 130J1 79 G 190J1A 95 E190J1A 95 96 FMS DATA LOADER H
136. RS SHALL NOT EXCEED 0 036 INCH AND SHALL NOT BE LESS THAN 0 005 INCH THE 3 32 INCH CABLE DIAMETER SHALL BE VERIFIED THESE ARE CRITICAL INSTALLATION REQUIREMENTS e Install two of four cable keepers supplied with new servo or removed in paragraph 25 A 1 c on the servo bracket at points of cable tangency to drum The other two keepers must be located at 90 degrees from the first two f Install retaining plate supplied with new servo or removed in paragraph 25 A 1 b on the end of the cable keepers and secure with four nuts and lock washers supplied with new servo or removed in paragraph 25 A 1 b Safety wire these four nuts with Low Mu Monel wire 0 020 inch in diameter and 4 inches long Adjustment Procedures Not Applicable Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 26 Procedure for the WC 880 Weather Radar Controller A Removal and Reinstallation Procedures 1 Remove WC 880 Weather Radar Controller a Disengage the Dzus fasteners on the unit b Slide the unit out of the aircraft mounting location and disconnect the cable connector 2 Reinstall WC 880 Weather Radar Controller a Mate the cable connector with the unit connector and slide the unit into the aircraft mounting location b Engage the Dzus fasteners on the unit B Adjustmen
137. S RS 422 TX L 46 FMS DATA LOADER RS 232 TX FMS DATA LOADER RS 232 RX BC DL RS 232 COMMON DISPLAY CONTROL 1 KD IOP RS 422 RX H SPARE CARD RESERVED SPARE CARD RESERVED V L 2 A 429 RCVR 21 L IOP RS 422 RX IAC IDENT 1 GND OPEN SPARE en H L SPARE no E IOP RS 422 TX L IDENT 0 GND OPEN WX CONTROL DATA 2 H IOP RS 422 RX L FMS DATA LOADER H 63 DATA IN FMS RS 422 RX L 190J1A 64 Connects To 123J1 H C190J1A 45 E190J1A 45 123J1 G C190J1A 46 E190J1A 46 FIGURE 8 3 115J1 5 115J1 4 FIGURE 8 2 59J1 e C190J1A 61 E190J1A 61 59J1 f C190J1A 62 E190J1A 62 123J1 T C190J1A 63 E190J1A 63 123J1 S C190J1A 64 E190J1A 64 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 0 BP Function Connector Pin Connects To FMS DATA LOADER 190J1A 65 CTS IN FMS RS 422 RX 66 ADF 2 67 429 RCVR 19 68 FIGURE 8 2 GND L GND HEAD UP DISPLAY BO SCA jocos iG aaa A 429 RCVR 8 70 24 FIGURE 8 2 GND L GND FGC RESERVED 71 SPARE FGC DISC 72 GND OPEN SPARE FWC DISC 73 GND OPEN SPARE FWC DISC 74 GND OPEN SPARE FWC DISC 75 GND OPEN SPARE FWC DISC 76 GND OPEN
138. SERVED IDENT RESISTOR R4 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED D14 RESERVED 170J1A D15 SEE 170J1A C10 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Function LAB LOCKOUT GNSSU NO A 429 RCVR GNSSU NO A 429 RCVR CTVAL1 CTVAL2 RESERVED RESERVED Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 1 cont LASEREF III Connector Pin 170J1A E1 E2 ES 2 E4 5 E6 E7 E8 9 Connects FIGURE 8 2 FIGURE 8 2 AC FAIL LOGIC AC TO BATT XFER RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED GNSSU 1 TIME MARK 1 H GNSSU 1 TIME MARK 1 L RESERVED RESERVED RESERVED RESERVED ASCB NO ASCB NO RESERVED RESERVED RESERVED RESERVED E10 E11 E12 E13 E14 E15 F1 F2 F3 F4 F5 149J1 19 2 PRI H 2 PRI L F10 F13 F11 F12 F13 F14 170J1A F15 FIGURE 8 1 SEE 170J1A F10 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Honeywell Function RESERVED GNSSU 2 TIME MA GNSSU 2 TIME MA RESERVED RESERVED RESERVED RESERVED RESERV
139. SERVED 136J1A 36 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Function RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 Connector Pin Connects To 136J1A 37 38 ID 1 CH GND OPEN ID 2 CH GND OPEN ID 3 CH GND OPEN SIGNAL GND 0 136J1A 72 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 10 BP Function Connector Pin Connects To 136 1 73 74 75 76 ASCB NO 1 PRI 77 DAU CHANNEL B S FIGURE 8 1 SEE 136J1A 77 ASCB NO 1 PRI H DAU CHANNEL A L S FIGURE 8 1 SIGNAL GROUND 1 CH A SIGNAL GND SIGNAL GROUND 2 CH A SIGNAL GND CHASSIS GROUND 101 102 28 VDC POWER CH A 103 28 VDC POWER CH A 104 FIGURE 8 6 DC POWER GND CH A 105 DC POWER GND DC POWER GND CH A 136J1A 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document S
140. SPARE 28 V ANN POWER H FIGURE 8 6 CHASSIS GND 28 V ANN POWER L DC POWER GND 0 5 V PANEL LIGHTING FIGURE 8 7 28 V PANEL LIGHTING SPARE NAV DATA OUT RS 422 XMTR NAV DATA TRM RDY RS 422 XMTR NAV DATA IN RS 422 RCVR NAV CLR TO SEND RS 422 RCVR NAV CLK IN RS 422 RCVR PERF DATA OUT RS 422 XMTR PERF DATA TRM RDY RS 422 XMTR 190J1C 72 190J1C 71 190J1C 59 190J1C 58 190J1C 52 190J1C 51 190J1C 49 190J1C 48 190J1C 64 190J1C 63 an ww anan Ro Ro Po Ro Po Ro Po Rope Ae Ae Ae Ae AER wwe wwe wwe wwe wwe B B B B B B B B B B B B B B wwe 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont CONTROL DISPLAY UNIT CDU NO 1 cont CD 810 Function Connector Pin Connects To PERF DATA IN 120J1 c RS 422 RCVR d PERF CLR TO SEND RS 422 RCVR PERF CLK IN RS 422 RCVR CDU VALID GND OPE i 190J1B 42 SPARE SPARE R PHOTO SENSOR OUT L PHOTO SENSOR OUT SPARE DIM CALIBRATION SPARE LAMP TEST GND OPEN FIGURE 8 7 SPARE SPARE ANNUN DIMMING ENABLE FIGURE 8 6 28V 0PEN ANNUN INTENSITY CONTROL FIGURE 8 7 0 28 V SPARE SPARE SPARE SPARE SPARE SPARE COLOR MONO TEST ENABLE GND OPEN SPARE SPARE SPARE 120J1 HH
141. TENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 Function Connector Pin Connects To CDU SYNC OUT 190J1C 69 C190J1A 19 GND OPEN E190J1A 19 TAG SYNC OUT 70 C190J1A 17 GND OPEN E190J1A 17 FMS CDU DATA IN ie 71 120J1 N FMS RS 422 RX H 72 S SPARE CARD RESERVED 73 SPARE CARD RESERVED 74 SPARE CARD RESERVED 75 LIGHTNING SENSOR H 76 429 RCVR 7 K 217 S FIGURE 8 2 SPARE H 78 S A 429 XMTR 2 f 79 FIGURE 8 2 SPARE CARD RESERVED 80 SPARE CARD RESERVED 81 SPARE FMS DISC OUT 82 GND OPEN SPARE FMS DISC OUT 83 GND OPEN SPARE FMS DISC OUT GND OPEN DU HDLC TX 1 H DU HDLC TX 1 L S S FIGURE 8 14 SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED SIGNAL GROUND SIGNAL GND SPARE CARD RESERVED SPARE IOP RS 422 TX LRN 1 A 429 RCVR 5 97 24 s 19001C 98 24 5 FLGURE 852 GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont 16 800 0 BP Function Connector Pin Connects To V L 1 190J1C 99 A 429 RCVR 3 100 FIGURE 8 2 DME 1 A 429 RCVR 2
142. Table 3 1 Interconnect Information cont DISPLAY UNIT NO 3 DU 870 Function Connector Pin Connects To 132J1 1 E135J1 1 13 24 E135J1 3 14 E135J1 2 H BRIGHTNESS POT L W H L W f 2 WX DIMMING L 3 15 RESERVED 4 RESERVED 5 RESERVED RESERVED SPARE RESERVED RESERVED RESERVED RESERVED 13 SEE 132J1 1 14 SEE 132J1 1 15 SEE 132J1 2 RESERVED 16 RESERVED 17 RESERVED BUS 3 H 19 BUS 3 NO TERM 1 20 FIGURE 8 14 BEZEL KNOB B0 21 115J1 37 C115J1 37 DU PWR DN GND OPEN 22 E135J1 4 E135J1 8 0 5 VDC EDGE H 23 FIGURE 8 7 LIGHTING L 24 LIGHTING GND BEZEL KNOB B1 25 115J1 38 C115J1 38 REMOTE LT SENSOR H 26 REMOTE LT SENSOR L 132J1 27 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 3 cont DU 870 Function Connector Pin Connects To DLS H 132J1 28 DLS 1 41 ALS 29 ALS 1 RESERVED RESERVED HDLC OUT RESERVED HDLC OUT BUS 3 TERM RESERVED BUS 2 FED BUS 2 NO TERM 1 DU VALID GND OPEN BUS 1 han BUS 1 NO TERM 1 REMOTE LT SENSOR GND FIGURE 8 14 FIGURE 8 14 SEE 132J1 28 SEE 132J1 29 RESERVED RESERVED BUS 4 TERM DU 3 PB5 RIGHT PB 115J1 41 GND OPEN C115J1 41 DU 3 PB4 115J1 40
143. This service is available both during and after warranty A Exchange Upon receipt of an exchange request Honeywell ships a fully certified unit The SPEX provided unit becomes the property of the customer The customer returns the faulty unit in exchange to the designated Honeywell Product Support Center where it becomes the property of Honeywell All exchange units are updated with the latest performance reliability MODs on an attrition basis while in the repair cycle Rental Upon receipt of a rental request Honeywell ships a fully certified unit The customer then ships the faulty unit to an authorized support center for service When the faulty unit has been serviced and installed the rental unit is returned to the designated Honeywell Product Support Center Warranty The SPEX 12 month warranty commences upon the purchase of an exchange unit by the customer at catalog list price Any exchange or repair action taken during the New Product or SPEX warranty period does not extend or otherwise affect the warranty expiration date Services provided for a failed unit under New Product warranty include Free repair and or free rental during repair of unit or Free exchange Services provided for a failed unit under SPEX warranty include Free repair and billable rental or Free exchange Services provided for a failed unit under repair warranty include Free rental if the customer paid for a billable
144. UT GND OPEN 190J1B 27 E190J1B 27 WX 2 RANGE DN OUT 28 24 C61J1 N GND OPEN 190J1B 28 E190J1B 28 WX 1 RANGE UP OUT C190J1B 29 24 61J1 L GND OPEN 190J1B 29 E190J1B 29 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To 0 WX 1 RANGE DN OUT C190J1B 30 24 GND OPEN 190J1B 30 E190J1B 30 0 SPARE DIO DISC OUT 31 28V 0PEN 0 SPARE DIO DISC OUT 28V 0PEN RSB RESERVED AP OFF HORN GND OPEN FIGURE 8 15 RSB RESERVED DP1 RESET GND OPEN SPARE DIO DISC OUT GND OPEN SPARE DIO DISC IN GND OPEN SPARE DIO DISC OUT GND OPEN RSB RESERVED CAUTION RESET GND OPEN FIGURE 8 11 CDU VALID GND OPEN C120J1 i SEC RADIO TUNE GND OPEN ALT ALERT HORN GND OPEN FIGURE 8 15 WX ON GND OPEN 5901 0 61J1 R 61 1 190J1B 45 E190J1B 45 WARNING ANNUN GND OPEN DU 2 REV GND OPEN RAD ALT TEST GND OPEN 4 FIGURE 8 13 EICAS RIGHT SEL GND OPEN E135J1 9 DAUI REV FIGURE 8 2 GND OPEN SG TEST IN C135J1 49 GND OPEN 115J2 16 C115J2 16 SPARE DIO DISC IN GND OPEN RSB RESERVED BC RESERVED BC RESERVED BC RESERVED 6 BC IDENT 2 C190J1B 57 SIGNAL GND GND OPEN 22 05 21 Sep 1 1
145. WER SUPPLY RESERVED 3 FMS DATA LDR CONNECTED 4 123J1 F GND OPEN POWER SUPPLY RESERVED 28V IAC POWER 28V IAC POWER FIGURE 8 6 28V IAC POWER FGC RESERVED TAC POWER RETURN TAC POWER RETURN DC POWER GND TAC POWER RETURN FGC RESERVED GC PANEL ANN VALID 28V 0PEN SPARE FGC DISC IN GND OPEN YD ACTUATOR EXTENDED YD ACTUATOR RETRACTED FGC RESERVED FGC RESERVED PITCH WHEEL 2 uo PITCH WHEEL 2 H NON SWITCHED LVDT RVDT EXCITATION TRIM POSITION H 4 TRIM POSITION L E190J1D 25 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pin Connects To FGC RESERVED E190J1D 26 0 DAU2 REV 27 GND OPEN 0 CAUTION ANNUN GND OPEN 28 I SG 2 REV GND OPEN 29 C135J1 40 1 SPARE DIO DISC IN 30 GND OPEN 1 PFD 2 OFF GND OPEN 31 C135J1 11 I SPARE DIO DISC IN 32 GND OPEN I FWC AP DISCONNECT IN FIGURE 11 GND OPEN RESERVED FWC DOWNLOAD IN PROGRESS 28V OPEN 1 SPARE DIO DISC IN GND OPEN RESERVED FWC ERASE IN PROGRESS 28V 0PEN TRUE REF SELECT GND OPEN SPARE FGC RVDT FIGURE 8 2 L ANALOG IN H FGC RESERVED PILOT EVENT MKR FIGURE 8 16 GND OPEN SPARE DIO DISC IN 42 GND OPEN I
146. X UNIT DESIGNATION CONNECTOR PIN MINIMUM WIRE GAUGE SIZE SHIELDING S Shield IS Inner Shield T Twisted 05 Outer Shield TO CONNECTION X 1 XX UNIT DESIGNATION EN CONNECTOR PIN All discrete signals include the logic type in parenthesis after the function name 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 4 1 3 3 Grounds GOOD GROUNDS ARE A KEY FACTOR IN A GOOD INSTALLATION Each ground should be run as a separate wire and terminated at one central point The following special requirements should be met Chassis grounds The bonding of an LRU chassis will be achieved via box mounting tray contact the tray being held at airframe ground potential by direct bolt down of the tray to the airframe The electrical bonding points on the aircraft must be guaranteed such that there is less than 10 milliohms resistance between the tray and the airframe For LRU s which do not have a mounting tray the preferred method of chassis bonding shall be achieved by direct contact of the LRU to airframe ground This method will require that the electrical bonding points on the aircraft are guaranteed such that there is less than 10 milliohms resistance between the LRU and the airframe An alternative method is to connect a minimum length cable strap 8
147. X BUS 1 TERM DU OVERTEMP GND OPEN DU WRAPAROUND H 190J1A 42 A 429 XMTR C190J1A 42 E190J1A 42 L S T S 190J1A 43 G C190J1A 43 E190J1A 43 RESERVED RESERVED WX BUS 3 131J1 70 WX BUS 3 NO TERM L 131J1 69 RESERVED RESERVED RESERVED WX BUS 2 131J1 75 WX BUS 2 NO TERM L L 131J1 74 SPARE WX BUS 1 WX BUS 1 NO TERM FIGURE 8 14 131J1 79 SEE 131J1 66 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 2 cont DU 870 10 BP Function Connector Pin Connects To 1 SIGNAL GROUND SIGNAL GND RESERVED RESERVED WX BUS 3 TERM RESERVED SPARE SPARE PORT SEL 3 GND OPEN 135J1 48 PORT SEL 2 GND OPEN 135J1 47 PORT SEL 1 GND OPEN I D 3 GND OPEN SIGNAL GND I D 2 GND OPEN I D 1 GND OPEN RESERVED CHASSIS GND RESERVED RESERVED RESERVED RESERVED SOFTWARE ENABLE GND OPEN SOFTWARE ENABLE 100 GND OPEN 28 VDC POWER 101 28 VDC POWER 102 FIGURE 8 6 28 VDC POWER 103 28 VDC POWER RETURN 104 28 VDC POWER RETURN 105 28 VDC POWER RETURN 131 1 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX
148. YSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 Function Connector Pi Connects To ITT AL 136J1B 1 ITT CH 2 3 WING FUEL QTY 4 WING FUEL QTY 25 N1 SPEED N1 SPEED FUEL FLOW DRUM FUEL FLOW COMMON L FUEL FLOW IMPELLER FUEL HTR TEMP EXC FUEL HTR TEMP EXC FUEL HEATER TEMP FUEL HEATER TEMP OIL PRESSURE L OIL PRESSURE TEMP EXC TEMP EXC TEMP TEMP OIL OIL OIL OIL STABILIZER POSITION STABILIZER POSITION STABILIZER POSITION RUDDER POSITION RUDDER POSITION RUDDER POSITION 136J1B 33 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 Function Connector Pin Connects To FLAPS POSITION H 136J1B 34 FLAPS POSITION W 35 FLAPS POSITION L 36 23 7 L N2 SPEED 38 L N2 SPEED 39 DEEC OUTPUT H 40 ARINC 429 CH A 41 C DEEC INPUT 42 ARINC 429 43 L VIBRATION INPUT 44 ARINC 429 45 R VIBRATION INPUT 46 ARINC 429 47 GPWS INPUT 48 ARINC 429 49 GPWS OUTPUT 50 ARINC 429 CH A 51 52 FLT DATA REC OUT 53 ARINC 573 717 FIGURE FIGURE FIGURE FIGURE FIGURE FIGURE 2 2 2 2 2 2
149. and slide the unit into the aircraft mounting location b Engage the Dzus fasteners on the unit B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 10 Procedure for the DU 870 Display Units A Removal and Reinstallation Procedures 1 Remove display unit Loosen two captive holding screws at ends of bezel assembly Gently pull bezel assembly straight away from display unit separating bezel and display unit connector Set bezel assembly aside Using a 3 16 inch Allen wrench loosen the jackscrew and separate the unit and tray connector s Gently lift the front of the display unit until the jackscrew latch clears the slot in the mounting tray Slide the display unit out of the tray 2 Reinstall display unit CAUTION WHEN PLACING THE UNIT ON THE MOUNTING TRAY DO NOT FORCE FIT IF MATING IS DIFFICULT REMOVE THE UNIT AND CHECK FOR CONNECTOR PINS THAT MAY BE BENT OR OUT OF ALIGNMENT ALSO VISUALLY CHECK THE ALIGNMENT OF THE RECEPTACLE ON THE MOUNTING TRAY Slide the display unit into the panel tray lifting the front of the display unit as necessary to ensure that the jackscrew latch engages the slot in the mounting tray Slide the display unit backwards until its connectors are fully engaged with t
150. aph 23 A 3 d on the servo bracket at points of cable tangency to drum The other two keepers must be located at 90 degrees from the first two e Install retaining plate Honeywell Part No 2518332 on the slotted end of the cable keepers using the four 5 16 inch long No 8 32 drilled fillister head screws removed in paragraph 23 A 3 c Safety wire these four screws with Low Mu Monel wire 0 032 inch in diameter and 4 inches long f Reinstall servo drive in accordance with paragraph 23 A 2 Adjustment Procedures Not Applicable Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 24 Procedure for the SM 725 Linear Actuator A Removal and Reinstallation Procedures 1 Remove linear actuator CAUTION DO NOT APPLY TORQUE BETWEEN OUTPUT ROD AND HOUSING DURING REMOVAL a Disconnect cable connector from actuator b Remove cotter pin bolt washer and nut securing fork end of actuator to airframe fitting c Remove cotter pin bolt washer nut and bushing securing rod end bearing of actuator to airframe fitting d If replacing the actuator remove the following I Unscrew rod end bearing Cut safety wire and remove nut and washer IN Unscrew fork end assembly Cut safety wire and remove nut and washer 2 Reinstall linear actuator INSTALLATI
151. ate Jets Tel 501 372 1501 Fax 501 372 5650 Wichita Kansas Tel 816 522 8172 Fax 816 522 2693 Eastern U S A Prospect Connecticut Tel 203 758 3252 Strongsville Ohio Tel 216 243 8877 Fax 216 243 1954 Fairfield New Jersey Mobil 201 822 9476 B Canada Montreal Quebec Tel 514 855 8063 Fax 514 636 6417 C South America Wheeling Illinois Tel 708 577 1753 Fax 708 459 8023 Altanta Georgia Tel 404 952 4445 Fax 404 984 8631 Reston Virginia Tel 703 620 4918 Fax 703 860 8985 Toronto Ontario Tel 416 375 3819 Fax 416 375 4531 San Jose Dos Campos Brazil Tel 55 123 25 1861 Fax 55 123 41 1675 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX D Europe and Africa Basingstoke England Munich Germany Tel 44 1256 51111 Tel 49 89 404072 Fax 44 1256 474932 Fax 49 89 401838 Toulouse France Paris France Tel 83 6212 1500 Tel 83 1447 38785 Fax 33 6130 0258 Fax 83 1447 49446 Rome Italy Tel 39 6 5037 294 Fax 39 6 5034 406 E Asia and Pacific Singapore Hong Kong Tel 65 542 1313 Tel 852 832 5681 Fax 65 542 1212 Fax 852 838 3280 Melbourne Australia Tel 61 3 330 1411 Fax 61 3 330 3042 22 05 21 Sep 1 1996 Use or disclosure of information on this page i
152. ation or at your facility as requirements dictate Refer to the list at the end of this section for corporate operations customer engineering locations telephone and fax numbers Training Honeywell s dedicated customer training staff is available to assist corporate operators in acquiring the technical skills and knowledge needed to operate and maintain Honeywell products Customer training conducts formal courses on corporate aircraft systems products at Honeywell s Customer Training Center in Phoenix Arizona and at selected locations worldwide Courses are scheduled annually based on customer interest and new aircraft delivery projections A regularly updated Honeywell Customer Training Schedule brochure gives full details of all training courses offered Honeywell offers the following level of training courses e Operational Pilot Training Flight Line Maintenance Training e Component Level Maintenance Training For full details and information on Honeywell training courses or a copy of the Honeywell Customer Training Schedule contact the Customer Training Department in Phoenix Arizona at Tel 602 436 8972 e Fax 602 436 4100 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 5 SYSTEM MAINTENANCE MANUAL FALCON 900EX Honeywell Honeywell Product Support Centers NOTE For further information on customer support
153. aximum allowable voltages are 18 0 and 32 2 V dc respectively The cyclic peak of ripple voltage to the mean level of the DC voltage shall be less than 2 0 volts NOTE For further information about aircraft power supply requirements refer to RTCA Radio Technical Commission for Aeronautics Specification D0 160C Power Distribution The Circuit Breaker configuration is divided into two categories Pilots and Copilots Pilot s and Copilot s Circuit Breakers should be driven by independent Aircraft Generators Interconnect Wiring The interconnect cabling shall be routed to minimize coupling with high current circuits including servo amplifier outputs and 28 V dc power inputs 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont Interconnect Format Each connection is typically shown as indicated below Wire terminations prefaced by the letter C indicate the copilot s side in a dual installation Wire terminations prefaced by the letter E indicate the third unit in a triple installation 2 3 4 5 6 DESCRIPTION FROM PIN AWG SHIELDING TO PIN S SERVO DRIVE 29J1A 1 22 Si Tagen secs 2901 2 SERVO DRIVE L 29J1A 2 INPUT OUTPUT DIGITAL BUS P POWER 1 0 INPUT OUTPUT DESCRIPTION OF SIGNAL FUNCTION FROM CONNECTION XX J1A X
154. be updated The loading of the new navigation data base can only be accomplished while the aircraft is on the ground Apply power to the data loader using the appropriate aircraft circuit breaker Push POWER switch on data loader The POWER LED shall light and after the powerup BITE sequence is completed the DATA LED shall light On data loader select LEFT or RIGHT or if the third FMS is installed select AUX Insert navigation database disc in data loader On the CD 810 Control Display Unit CDU select the DATA LOAD page from the NAV INDEX page 2 On the DATA TO BE LOADED page select NAV DB On the TRANSFER OF NAV DB page select FR LOADER On the CONFIRM TRANSFER OF NAV DB page confirm selection by selecting YES or NO Monitor of loading progress In the case of the worldwide database the IAC FMS prompts for insertion of more than one disc The IAC FMS automatically begins reading the next disc When complete the message DB TRANSFER COMPLETE is displayed and the IAC FMS does a restart NOTE The data load process must be repeated from the beginning when power is interrupted ABORT is selected or other problems that stop the loading process occur Repeat steps d through j for each IAC FMS that needs to be updated Remove disc and turn off data loader Remove from aircraft if not permanently installed 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title
155. changed by the nose jack there is no roll change introduced in the original roll level This is very important in order for the yaw alignment correction to be accurate 4 While the airplane is on jacks small changes in the level position may be introduced which could affect the accuracy of the alignment procedure Such changes could occur due to wind through an open hangar door or personnel moving around inside or on the airplane Once the airplane level has been achieved no changes to the airplane loading or position should be made 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX b If applicable place the mounting tray on the surface to which the tray will be mounted and secure the tray snugly with the four sets of mounting hardware The two mounting holes at the blower end of the rack are elongated to provide for yaw adjustment The mounting bolts for these two elongated holes should be centered in the slots This software method is capable of correcting for as much as 40 degrees of mechanical tray misalignment c Slide the UG5046 Leveling Fixture into the three guide pins of the mounting tray Secure the leveling fixture to the mounting tray by tightening the two thumbwheel clamps over the support hooks Hand tighten only NOTE Figure 4 4 represents the UG5046 Leveling Fixture The sensitivity of
156. connector s 2 Reinstall DC 840 Display Controller a b Mate the cable connector s with the unit connector s and slide the unit into the aircraft mounting location Engage the Dzus fasteners on the unit B Adjustment Procedures Not Applicable C Repair Procedures 1 Replacement of the HDG TRK Knobs and PUSH SYNC Pushbutton NOTE The pushbutton setscrews are reached through access holes in the outer knob Rotate the outer knob fully CCW Use a 0 048 inch O D 6 flute Bristol wrench to loosen the setscrews in the outer knob Rotate outer knob until access hole lines up with setscrews on inner PUSH SYNC pushbutton and loosen two setscrews Slide the knob and pushbutton off of the shaft Rotate knob to HDG position and loosen setscrews Slide knob off of shaft On new knobs and pushbutton make sure that the setscrews are out far enough to allow knobs and pushbutton to slide onto shaft Apply retaining compound to setscrews Slide the selector knob onto the shaft Ensure that the space between the knob and front panel is approximately 0 030 inch 0 8 mm and tighten setscrews Slide the outer knob onto the shaft Do not tighten setscrews 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE MANUAL FALCON 900EX Honeywell Slide the PUSH SYNC pushbutton onto the shaft Align the access h
157. ction Connector Pin Connects To 0 GNSSU FAULT 149J1 1 0 RS 232 XMTR ne 1 RS 232 RCVR 3 FIGURE 8 3 DATA LOADER INPUT 4 ARINC 429 15 SDI 2 5 SDI 1 36 PRI DADC INPUT 6 ARINC 429 7 PROG DISCRETE RETURN 8 149J1 5 TIME MARK 2 9 C170J1A G2 TIME MARK 2 22 C170J1A G3 SEC DADC INPUT 10 ARINC 429 11 DATA LOAD MODE DISCRETE 12 TIME MARK 3 H 13 S E170J1A F4 TIME MARK 3 L 14 S T E170J1A F5 GND 15 GEN PURP INPUT 1 16 ARINC 429 17 PRI IRS FMC IN 18 ARINC 429 37 S T FIGURE 8 2 TIME MARK 1 19 170J1A F4 TIME MARK 1 20 S T 170J1A F5 429 OUT HS LS SELECT 21 149J1 22 SEE 149J1 9 L 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont GLOBAL NAVIGATION SATELLITE SENSOR GNSSU NO 1 GNSSU Function Connector Pin Connects To GEN PURP INPUT 2 149J1 23 ARINC 429 41 GNSSU OUTPUT 2 24 ARINC 429 25 SEC IRS FMC IN 26 ARINC 429 27 ATR GROUND 28 GNSSU OUTPUT 3 29 ARINC 429 30 CMC IN 31 ARINC 429 32 CHASSIS GROUND 33 DC POWER GND DC POWER GND 28 VDC POWER FIGURE 8 6 SEE 149J1 5 SEE 149J1 18 FIGURE 8 2 GNSSU OUTPUT 1 H DAS uds sd see ARINC 429 L DADC IN 419 429 SELECT 149J1 41 SEE 149J1 23
158. ctions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To FGC RESERVED C190J1D 26 0 DAU2 REV 27 GND OPEN 0 CAUTION ANNUN GND OPEN 28 I SG 2 REV GND OPEN 29 C135J1 39 1 SPARE DIO DISC IN 30 GND OPEN 1 PFD 2 OFF GND OPEN 31 C135J1 10 I SPARE DIO DISC IN 32 GND OPEN I FWC AP DISCONNECT FIGURE 8 11 GND OPEN RESERVED FWC DOWNLOAD IN PROGRESS 28V OPEN 1 SPARE DIO DISC IN GND OPEN RESERVED FWC ERASE IN PROGRESS 28V 0PEN TRUE REF SELECT GND OPEN SPARE FGC RVDT FIGURE 8 2 L ANALOG IN H FGC RESERVED PILOT EVENT MKR FIGURE 8 16 GND OPEN SPARE DIO DISC IN 42 GND OPEN IAC 1 OVERHEAT 43 190J1B 67 GND OPEN 190J1D 43 E190J1D 43 CHECK PFD ANNUN GND OPEN 44 FIGURE 8 15 SG 1 REV GND OPEN 45 135J1 39 CHASSIS GROUND C190J1D 46 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 IO BP Function Connector Pin Connects To 0 SPARE DIO DISC OUT C190J1D 47 28V 0PEN 1 TAC 2 OVERHEAT GND OPEN 48 C190J1B 67 190J1D 48 E190J
159. ctor Pin Connects To FGC RESERVED 190J1D 26 0 DAU2 REV 27 GND OPEN 0 CAUTION ANNUN GND OPEN 28 I SG 2 REV GND OPEN 29 C135J1 41 1 SPARE DIO DISC IN 30 GND OPEN 1 PFD 2 OFF GND OPEN 31 135 1 9 1 SPARE DIO DISC IN 32 GND OPEN 1 DISCONNECT FIGURE 8 11 GND OPEN RESERVED FWC DOWNLOAD IN PROGRESS 28V 0PEN 1 SPARE DIO DISC IN GND OPEN RESERVED FWC ERASE IN PROGRESS 28V 0PEN TRUE REF SELECT GND OPEN SPARE FGC RVDT FIGURE 8 2 L ANALOG IN H FGC RESERVED PILOT EVENT MKR FIGURE 8 16 GND OPEN SPARE DIO DISC IN 42 GND OPEN IAC 1 OVERHEAT 43 190J1B 67 GND OPEN C190J1D 43 E190J1D 43 CHECK PFD ANNUN GND OPEN 44 FIGURE 8 15 SG 1 REV GND OPEN 45 135J1 41 CHASSIS GROUND 190J1D 46 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pin Connects To 0 SPARE DIO DISC OUT 190J1D 47 28V 0PEN 1 TAC 2 OVERHEAT GND OPEN 48 C190J1B 67 C190J1D 48 E190J1D 48 SPARE DIO DISC OUT 49 28V 0PEN GC PANEL STROBE OUT L 50 GC PANEL STROBE OUT H 51 1101 5 L_GND FGC RESERVED 52 SG 3 REV GND OPEN 53 E135J1 44 YD LVDT FEEDBACK L 54 14J1 M C190J1D 54
160. d 1 Preferred RT 300 Zero Ground Adjustment a Connect cable Figure 4 5 in line with the aircraft cable and the RT 300 b Check that the RT 300 transmit and receive ports J2 and J3 are connected to the antennas c Connect a digital voltmeter DVM to the cable meter leads d Apply power to the RT 300 e Adjust the potentiometer that is accessible through hole in front panel of RT 300 for 0 2 mV indication on DVM f Remove power and disconnect adjustment cable g Connect aircraft cable to RT 300 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell anu FALCON 900EX TO AIRCRAFT TO RT 300 CABLE lolol N x2 caovomnmuzzr c xc cromnmmoonusorvmr A B C D E F G H J K L M N P R S T U v w x Y 2 b MS3126F16 26S 4 MS3121F16 26P NOTES 1 ALL WIRING 22 AWG EXCEPT AS NOTED 2 WIRING FOR PINS b AND c IS 20 AWG 3 LENGTH OF CABLE IS SIX INCHES 4 LENGTH OF DVM LEADS ARE AS REQUIRED CONNECT PLUG TO LEADS AS REQUIRED TO CONNECT TO DVM AD 31291 Figure 4 5 RT 300 Zero Adjustment Cable 2 Alternate RT 300 Zero Ground Adjustment a Apply power to the RT 300 b Adjust the potentiometer that is accessible through hole in front panel of RT 300 until a positive radio altitude is displayed on one of the PFDs c Adjust the potentiometer for zero foot dis
161. degrees If not adjust the elevation feedback potentiometer R1 for 0 1 4 degrees Press and hold the IRS TEST switch pushbutton This simulates 15 degrees of nose up pitch and 5 degrees of right roll Verify that the antenna tilts down 15 2 degrees Release IRS TEST switch pushbutton Pull out GAIN knob to select variable gain This places the WU 870 in the roll calibration mode Press and hold IRS TEST switch pushbutton Verify that the antenna tilts up 5 1 degrees Release IRS TEST switch pushbutton Remove power from the radar Set SCAN and XMTR toggle switches on the WU 870 housing to ON away from antenna Apply aircraft power as necessary Verify in the SBY mode that the antenna is tilted up 15 2 degrees 2 Adjust WU 870 Antenna and Receiver Transmitter in flight a b At an altitude of 10 000 feet 3 048 meters above the ground or greater establish a wings level cruise altitude On the WC 880 Weather Radar Controller select WX mode variable GAIN and RCT OFF Select 100 NM range using cockpit mounted range switches Observe VAR on MFD Adjust the antenna tilt down until a fairly solid band of ground clutter is visible Select RCT on off on off within three seconds by setting RADAR knob between RCT and WX VAR should not be displayed This puts the radar in the roll compensation mode 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the ti
162. e is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont 127 OHM AA m CONN NO 2 gt CC FIGURE 3 190J1B 15 A E190J1B COUPLER 1 13 170J1A C190J1D F10 104 106 E170J1A 4 C170J1A F10 C10 9J1 65 7j me BUT l 34 136J2A 137J1A 94 94 96 96 77 77 sa D as 127 136J2B 127 OHM AD 41490 NOTE Shielding connections assume the stub is constructed as shown in Figure 5 2 If this method of stub construction is not feasible the stub shield must be connected to ASCB bus shield at one end and connected to aircraft ground at the other end as shown in Figure 5 1 ASCB Connections Bus 2 Primary and Bus 2 Backup Figure 8 1b 22 05 21 Sep 1 1896 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont C190J1A c2 1 i E190J1A 20 T 2 peso 9 E190J1C 4 abs c UD eee LI
163. e sure that hold down hook engages boss on MADC and using a 3 16 inch Allen wrench tighten jackscrew d Mate cable connector and unit connector e Connect pitot and static lines and perform appropriate pitot static leak check as instructed in the Aircraft Maintenance Manual B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 5 Procedure for the BL 871 Bezel Assembly A Removal and Reinstallation Procedures 1 Remove bezel assembly a Loosen two captive holding screws at ends of bezel assembly b Gently pull bezel assembly straight away from display unit separating the bezel and display unit connectors 2 Reinstall bezel assembly a Align bezel assembly on the display unit so bezel and display unit connectors mate b Tighten the captive screws B Adjustment Procedures Not Applicable C Repair Procedure Replacement of the BL 871 Bezel Assembly Set Knob 1 Loosen both setscrews in the knob with a 1 16 inch Allen wrench 2 Slide knob off of shaft 3 On new knob make sure that the setscrews are out far enough to allow the knob to slide onto the shaft Apply retaining compound to setscrews 4 Slide the knob onto the shaft 5 Make sure that the space between the knob and the bezel is approximately 0
164. ect to the restrictions on the title page of this document 10 BP 1 SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 4 cont DU 870 Function Connector Pin Connects To C131J1 79 SEE C131J1 66 SIGNAL GROUND SIGNAL GND RESERVED RESERVED WX BUS 3 TERM RESERVED SPARE SPARE PORT SEL 3 GND OPEN 135J1 48 PORT SEL 2 GND OPEN 135J1 47 PORT SEL 1 GND OPEN I D 3 GND OPEN I D 2 GND OPEN 1 I D 1 GND OPEN SIGNAL GND RESERVED CHASSIS GND RESERVED RESERVED RESERVED RESERVED SOFTWARE ENABLE GND OPEN SOFTWARE ENABLE GND OPEN 28 VDC POWER 28 VDC POWER FIGURE 8 6 28 VDC POWER 28 VDC POWER RETURN 28 VDC POWER RETURN DC POWER GND 28 VDC POWER RETURN C131J1 106 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont REVERSIONARY CONTROLLER NO 2 RC 820 Function Connector Pi Connects To COPILOT PFD C135J1 1 C130J1 1 BRIGHTNESS POT 2 C130J1 14 3 C130J1 13 COPILOT MFD 4 BRIGHTNESS POT zb C131J1 14 6 S C131J1 13 COPILOT PFD ON GND OPEN 7 COPILOT PFD OFF GND OPEN 8 C130J1 22 COPILOT PFD OFF GND OPEN 9 190J1D 31 COPILOT PFD OFF GND OPEN 10 C190J1D 31 COPILOT PFD OFF GND OPEN 11 E190J1D 31 AUTO EICAS REV 3 GND
165. ects To FGC RESERVED E190J1C 45 FGC RESERVED 46 FGC RESERVED 47 FMS CDU DTR OUT 48 S E120Jd1 V FMS RS 422 TX 49 S T S E120J1 U L_GND FGC RESERVED 50 FMS CDU DATA OUT 51 S EI20J1 T FMS RS 422 TX 52 S E120J1 S SPARE CARD RESERVED 53 SPARE CARD RESERVED 54 CROSS CHANNEL SYNC OUT 55 GND OPEN SPARE FGC DISC IN 56 28V 0PEN FGC RESERVED 57 FMS CDU CTS IN 58 S 12001 FMS RS 422 RX S E120J1 P SPARE FGC ANALOG IN 60 SPARE FGC ANALOG IN 61 FGC RESERVED 62 FMS CDU CLOCK OUT 63 E120J1 X FMS RS 422 TX 64 S E120J1 W G TCAS 65 A 429 RCVR 6 66 5 FIGURE 8 2 SPARE CARD RESERVED 67 SPARE FMS DISC OUT 68 GND OPEN CDU SYNC OUT 69 190J1A 32 GND OPEN C190J1A 32 TAG SYNC OUT E190J1C 70 190J1A 18 GND OPEN C190J1A 18 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 Function Connector Pin Connects To E190J1C 71 24 S T S E120J1 N 72 24 S E120J1 M FMS CDU DATA IN L FMS RS 422 RX H SPARE CARD RESERVED SPARE CARD RESERVED SPARE CARD RESERVED LIGHTNING SENSOR A 429 RCVR 7 FIGURE 8 2 SPARE 429 XMTR 2 5 FIGURE 8 2 SPARE CARD RESERVED SPARE CARD RESERVED SPARE FMS DISC OUT GND O
166. ed CB3 1 A429 LRN1 Config CB3 2 A429 LRN1 Config CB3 3 A429 LRN1 Number All combinations allowed CB3 4 A429 LRN1 Number CB3 5 of Autopilots F900EX always has 2 autopilots CB3 6 AFIS Installed AFIS is optional on F900EX CB3 7 1 CB4 0 A429 LRN2 Config All combinations allowed 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISCRETE BYTE BIT GENERIC DESCRIPTION CB4 1 A429 LRN2 Config CB4 2 A429 LRN2 Config CB4 3 A429 LRN2 Number combinations allowed CB4 4 A429 LRN2 Number CB4 5 FMS Mode 2 combinations allowed CB4 6 FMS Mode 1 CB4 7 1 CB5 0 A429 LRN3 Config combinations allowed CB5 1 A429 LRN3 Config CB5 2 A429 LRN3 Config CB5 3 A429 LRN3 Number All combinations allowed CB5 4 A429 LRN3 Number CB5 5 Sensor 1 Type Sensor 1 is always an IRS on F900EX CB5 6 Sensor 2 Type Sensor 2 is always an IRS on F900EX CB5 7 1 CB6 0 Sensor 3 Type Sensor 3 if installed is always an IRS on F900EX CB6 1 Sensor 4 Type Sensor 4 is not allowed on F900EX CB6 2 Radio Type 3 F900EX will always have A429 CB6 3 Radio Type 2 radios CB6 4 Radio Type 1 CB6 5 of ATCs 2 F900EX will always have 2 CB6 6 of ATCs 1 ATCs CB6 7 1 CB7 0 TCAS Installed TCAS is optional on F900EX CB7 1 of ADFs 2 F900EX will always have 2 ADFs CB7 2 of AD
167. ely wherever possible should not pass through common connectors or feedthroughs and should not be installed in high risk areas such as wing leading edges engine shrapnel path etc 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont WX Display Unit Bus Interface The WX DU buses provide Weather Radar data from the WX unit to the DUs The following paragraphs define the electrical interface requirements for the WX DU interconnect The WX DU transmission lines shall have a characteristic impedance of 70 7 ohms The characteristic capacitance shall be 30 picofarads foot max The maximum attenuation shall be 1 4 decibels 100 feet when measured at 1 MHz Honeywell Part No 3718911 1 cable or equivalent shall be used Note ASCB type cable cannot be used The preferred method of WX DU interconnect is to provide the bus termination resistors in the aircraft wiring This allows any display or displays to be removed and not affect operation of the remaining displays This method is shown in Figure 6 4 and Figure 8 14 WX 1 MHz PICTURE BUS NOTES 1 THE STUB SHEILDING CAN BE ELIMINATED BY CONSTRUCTING THE STUB AS SHOWN IN FIG 5 2 CABLE HONEYWELL PART NO 3718911 1 OR EQUIVALENT CHARACTERISTIC IMPEDANCE 70 7 OHMS CHARACTERISTIC CAPACITANCE 30 P
168. ent and recommends a circuit breaker The circuit breakers were selected assuming the following size breakers are available 1 2 5 5 7 5 10 and 15 amps Table 4 2 Circuit Breaker Selections Max Power Worst Case Circuit Minimum Wire Maximum Wire watts Voltage for Breaker Size Required Size in LRU Max Power in Aircraft Connector volts 24 aa NEED dp l RE MI a a L 94 I Laser Ref III steady state Laser Ref III start up Wire in aircraft is larger than LRU connector will accept Wiring in aircraft should use a single wire from the circuit breaker to near the LRU connector This wire should then be spliced to one or more wires as appropriate for a given LRU of a gauge that can be accepted by the LRU connector similar method could be used for the power grounds or several wires of a gauge allowed by the LRU connector could be run individually to ground First row is for main power for unit Second row is for annunciator power Total unit power is the sum of these values and is supplied from a single circuit breaker Estimated power 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont AVIONICS STANDARD COMMUNICATION BUS ASCB VERSION C The ASCB is the primary communication path between majo
169. ews e Slide the outer knob onto the shaft ensuring that the white line aligns with the NORM position f Ensure that space between knob and front panel is approximately 0 030 inch 0 8 mm g Tighten the knob setscrews h Recheck spacing between knob and front panel to ensure that knob has not slipped during installation i Slide the inner knob onto the shaft making sure that the knob does not rub against the outer knob j Tighten the knob setscrews k Recheck to make sure that the inner knob has not slipped during installation and is not rubbing against the outer knob 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX 2 Replacement of the SG Knob and PUSH TEST Pushbutton NOTE The pushbutton setscrews are reached through access holes in the select knobs a Rotate the outer knob to the NORM position b Use a 0 048 inch O D 6 flute Bristol wrench to loosen the setscrews in the outer knob c Rotate outer knob until access hole lines up with setscrews on inner PUSH TEST pushbutton and loosen two setscrews d Slide the knob and pushbutton off of the shaft e On new knob and pushbutton make sure that the setscrews are out far enough to allow knob and pushbutton to slide onto shaft Apply retaining compound to setscrews f Slide the outer knob onto the shaft
170. ews h Recheck spacing between knob and front panel to ensure that knob has not slipped during installation i Slide the inner knob onto the shaft making sure that the knob does not rub against the outer knob and that the line aligns with the OFF REV position j Tighten the knob setscrews k Recheck to make sure that the inner knob has not slipped during installation and is not rubbing against the outer knob 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 21 Procedure for the RC 841 Reversionary Controller A Removal and Reinstallation Procedures 1 Remove RC 841 Reversionary Controller a Remove and set aside four flat head mounting screws b Slide unit out of panel and disconnect cable connector 2 Reinstall RC 841 Reversionary Controller a Mate cable connector with unit connector and slide unit into panel b Secure unit with four flat head mounting screws that were previously set aside B Adjustment Procedure Not Applicable C Repair Procedures 1 Replacement of the EICAS DSPLY and XFR DIM Knobs a Set outer knob to NORM position b Use a 0 048 inch O D 6 flute Bristol wrench to loosen the setscrews c Slide the knobs off of the shaft d On new knobs make sure that the setscrews are out far enough to allow the knob to slide onto the shaft Apply retaining compound to setscr
171. flute Bristol wrench to loosen the setscrews on each knob Slide the knobs off the shaft On new knobs make sure that the setscrews are out far enough to allow knobs to slide onto shaft Apply retaining compound to setscrews Slide the selector knob onto the shaft so notch aligns with DH Ensure that the space between the knob and front panel is approximately 0 030 inch 0 8 mm and tighten setscrews Slide the inner knob onto the shaft making sure that the knob does not rub against the selector knob Tighten the knob setscrews Recheck to make sure that the inner knob has not slipped during installation and is not rubbing against the selector knob 4 Replacement of the ASEL Knob Loosen the setscrews with a 0 048 inch O D 6 flute Bristol wrench Slide the knob off of the shaft On new knob make sure that the setscrews are out far enough to allow knob to slide onto the shaft Apply retaining compound to setscrews Slide the knob onto the shaft Ensure that the space between the knob and the front panel is approximately 0 030 inch 0 8 mm Tighten the knob setscrews Visually check the spacing between the knob and front panel to ensure that the knob has not slipped during installation 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX 12 Procedure for the Global Navigation Sy
172. formation cont HGS Installed 1 Discrete HGS Installed Config 67 HGS Not Installed 0 HGS Installed 1 GPWS Installed 1 Discrete GPWS Installed Config 72 GPWS Not Installed 0 GPWS Installed 1 FD Operation Mode 2 Discretes FD Operation Mode Config 76 Config 75 Bezel Selectable Independent FD 0 No Bezel Control Cross Pointer 0 Bezel Selectable Same FD on both sides synch 1 No Bezel Control Single Cue 1 Aircraft Identification 6 Discretes Aircraft Ident Config 83 Config 82 Config 81 Config 80 Config 79 Config 78 FALCON 900EX 0 0 1 0 1 0 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX TABLE OF CONTENTS SECTION 4 SECTION PARAGRAPH TITLE PAGE 4 MAINTENANCE PRACTICES 4 1 1 General torpis ear rr EE de ARE EXIMIAM EON EET ERE E ee MERI 4 1 2 Equipment and Materials 4 1 3 Procedure for the AT 300 Radio Altimeter Antenna 4 2 4 Procedure for the AZ 840 Micro Air Data Computer MADC 4 4 5 Procedure for the BL 871 Bezel Assembly 4 5 6 Procedure for the CD 810 Control Display Unit 4 6 T Procedure for the DA 800 Data Acquisition Unit DAU 4 7 8 Procedure for the DC 840 Displa
173. ge of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 2 cont DU 870 Function Connector Pin Connects To DLS H 131J1 28 24 s 130J1 29 DLS L 41 24 S 130d1 42 GNo ALS H 29 24 S ALS L 24 5 GND RESERVED RESERVED HDLC OUT RESERVED HDLC OUT BUS 3 TERM RESERVED BUS 2 FED BUS 2 NO TERM 1 DU VALID GND OPEN BUS 1 han BUS 1 NO TERM 1 REMOTE LT SENSOR GND SEE 131J1 28 SEE 131J1 29 RESERVED RESERVED BUS 4 TERM DU 2 PB5 RIGHT PB 115J1 32 GND OPEN C115J1 32 DU 2 PB4 115J1 31 GND OPEN C115J1 31 RESERVED BUS 2 TERM 49 DU 2 PB3 50 115J1 28 GND OPEN C115J1 28 DU 2 PB2 51 115J1 27 GND OPEN C115J1 27 BUS 1 TERM 52 REM LT SENSOR 53 REM LT SENSOR 131J1 54 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 2 cont DU 870 Function Connector Pin Connects To RESERVED 131J1 55 RESERVED 56 RESERVED 57 BUS 4 H BUS 4 NO TERM L 59 FIGURE 8 14 DU 2 PB1 60 115J1 26 GND OPEN C115J1 26 WX BUS 2 TERM 61 DU 2 PBO LEFT PB 115J1 25 GND OPEN C115J1 25 KNOB PB COMMON SIGNAL GND W
174. ge of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 wore Function Connector Pin Connects To LT ENG IGN 28 0 136 2 37 RT ENG IGN 28 0 38 SPARE 28 0 239 WING ANTI ICE CMD 28 0 40 FLAPS 7 DEG SEL 28 0 41 FLAPS 20 DEG SEL 28 0 42 FLAPS 40 DEG SEL 28 0 43 LT ENG START 28 0 44 END ITEM TEST 28 0 45 RT ENG START 28 0 46 LT BUS VOLTAGE NORM 28 0 47 RAD ALT 1 VALID 28 0 Ro Po Ro PO PS PS PO PO AAA HAHAHAHAHA annan ID 1 CHB GND OPEN ID 2 CHB GND OPEN ID 3 CHB GND OPEN SIGNAL GND 0 136J2A 72 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 1 cont DA 800 10 BP Function Connector Pin Connects To 13622A 73 74 75 76 ASCB NO 2 PRI 77 DAU CHANNEL B S FIGURE 8 1 SEE 136J2A 77 ASCB NO 2 PRI H DAU CHANNEL A L S FIGURE 8 1 SIGNAL GROUND 1 CH B 99 SIGNAL GND SIGNAL GROUND 2 CH B 100 SIGNAL GND CHASSIS GROUND 101 102 28 VDC POWER CH B 103 28 VDC POWER CH
175. he mating connectors of the mounting tray Tighten the jackscrew with a 3 16 inch Allen wrench Reinstall bezel assembly I Align the bezel assembly on the display unit D Tighten the captive screws 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Adjustment Procedure Not Applicable Repair Procedure Not Applicable Cleaning Procedure Cleaning of the Display Unit Faceplate Filter NOTE The display unit faceplate is protected by a filter which reduces reflections It is sturdy but it is not indestructible 1 Inspect the outside surface for foreign material and variations in optical quality 2 Particles of grit dirt or sand are to be removed with pressurized dry air or a soft camel hair brush 3 Dampen a clean piece of lint free cloth with isopropyl alcohol or ammoniated cleaner Do not use household paper towels 4 Carefully rub the unclean portion of the filter with the damp cloth 5 Repeat steps 2 and 3 as necessary until the filter is clean 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 11 Procedure for the GC 810 Flight Guidance Controller A Removal and Reinstallation Procedures 1 Remove GC 810 Flight Guidance Controller a D
176. he DATA TO BE LOADED page select CUSTOM DB On the TRANSFER OF CUSTOM DB page select TO LOADER or FR LOADER depending on whether you are transferring data from or to the data loader On the CONFIRM TRANSFER OF CUSTOM DB page confirm selection by selecting YES or NO Monitor of loading progress When complete the message DB TRANSFER COMPLETE is displayed The IAC FMS does a restart in the case where the custom database was loaded from the data loader NOTE The data load process must be repeated from the beginning when power is interrupted ABORT is selected or other problems that stop the loading process occur Remove disc and turn off data loader Remove from aircraft if not permanently installed 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 3 Transferring the Navigation or Custom Database Between IACs The custom or navigation database can be transferred from one IAC to the other IAC Only the custom database can be transferred in flight In order to transfer data both ACs must be turned on and have compatible software versions All of the following steps can be completed from just one of the CD 810 Control Display Units a b On the CD 810 Control Display Unit CDU select the DATA LOAD page from the NAV INDEX page 2 On the DATA TO BE LOADED page select CUSTOM DB NAV DB
177. he aircraft using leveling device Honeywell Part No UG5046 in accordance with one of the following two methods specified in paragraphs 18 B 1 and 2 NOTE These procedures outline several methods of tray alignment The user or installer should ensure that any of the following methods do not conflict with the aircraft manufacturers recommendations or procedures 1 Recommended Leveling Procedure Method 1 a Place the airplane on jacks and level the airplane in accordance with the airplane manufacturers procedures The airplane should be leveled to within 0 2 degree or less NOTES 1 It may be desirable in some situations for ease of performing this procedure and for safety reasons to have the aircraft main gear remain on the floor while pitching the aircraft If this is the case the roll leveling of the aircraft may be adjusted by lowering one of the main gear struts or lowering the tire pressure of one of the main tires or both 2 The leveling of the mounting tray can be no better than the leveling of the airplane Care should be exercised during the leveling of the airplane to ensure that the best possible airplane leveling is achieved 3 The accuracy of the tray heading alignment is dependent on the placement of the jacks The wing jacks should be placed such that they are an equal distance back from the nose jack and perpendicular to the longitudinal axis of the airplane so that when the airplane pitch attitude is
178. he restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX TABLE OF CONTENTS SECTION 6 SECTION PARAGRAPH TITLE PAGE 6 HONEYWELL SUPPORT 6 1 1 Worldwide Exchange Rental Program for Corporate Operators 6 1 2 Test Equipm nt c OS wu Reg rd EREMO ee 6 5 3 Customer Engineering 6 5 4 Training ug quce Roa xem Bw A Bi AE ern XR Et 6 5 5 Honeywell Product Support 6 6 6 Corporate Operations Customer Engineering Locations 6 8 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Blank Page 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX SECTION 6 HONEYWELL SUPPORT Worldwide Exchange Rental Program for Corporate Operators Honeywell s SPEX program is a worldwide exchange rental service for corporate operators It provides an extensive service for LRU end item products complementing our worldwide support center network An inventory of more than 8000 spare components ensures that your Honeywell equipped aircraft will be returned to service promptly and economically
179. hes This 6 inch length consists of 4 inches of unshielded ASCB cable plus 2 inches of 24 AWG stranded wire The 2 inch length of 24 AWG wire connects to the LRU connector at one end and the splice of the two ASCB wires at the other end This 2 inch extension wire is used because more than one ASCB wire cannot be inserted into an LRU connector pin The 6 inch stub wires shall be twisted as shown in Figure 5 2 Butt splices with solder rings will be utilized for all stub interconnections ref Figure 5 2 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont The ASCB bus shield connections at each stub shall be accomplished with a butt splice which will provide a maximum shield to shield connection of 0 3 inches If a stub shield is used its maximum length is 10 inches Connect the stub shield to the bus shield as shown in Figure 5 1 with a butt splice of minimum length less than 2 inches 20 AWG wire All exposed wires at the splice and wires used to connect shields at the splice shall be covered with an overbraid material The overbraid material shall then be tied to the shield or airframe ground There shall be no unshielded portion of the ASCB Shields should be bonded to the outer shell of each LRU The Bus shields shall be grounded to the airframe ground a
180. his document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont PILOT S COPILOT S AT DISC SW AT DISC SW E190J1A 87 E190J1A 102 190J1B 102 C190J1B 102 E190J1B 102 PILOT S COPILOT S AP DISC SW AP DISC SW 1101 71 11J2 71 190J1A 87 C190J1A 87 190J1D 33 C190J1D 33 E190J1D 33 PILOT S GA TO SW S 11J1 59 COPILOT S GA TO SW PILOT S TCS SW L 11J1 60 COPILOT S TCS SW PILOT S MASTER TPAUTION 190J1B 41 C190J1B 41 COPILOT S E190J1B 41 MASTER CAUTION AD 41500 R1 Miscellaneous Switches Figure 8 11 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont 190J1B C190J1B e IAC 1 IAC 2 PILOT S 87 87 PILOT S STICKSHAKER STICKSHAKER 190J1D C190J1D COPILOT S 93 93 COPILOT S STICKSHAKER STICKSHAKER LI Il NO 1 STALL NO 2 STALL WARNING 28VDC STALL 28VDC STALL WARNING COMPUTER COMPUTER AD 41501 Stick Shakers Figure 8 12 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont RAD ALT RT 13618 DAU 1 RADALT
181. ig 22 Spare Low Speed IRS High Speed Omega Low Speed Spare High Speed GPS Low Speed GPS High Speed Spare High Speed Spare Low Speed A429 LRN 2 Number 2 Discretes A429 LRN 2 Number Config 26 Config 25 LRN 0 0 LRN 1 0 LRN 2 1 LRN 3 1 FMS Operational Mode 2 Discretes FMS Operational Mode Config 28 Config 27 Dual 0 Independent 0 Single 1 CDU Mode Control 1 NOTE If the Dual Mode Control is selected the dynamic discretes Initiated Transfer Transmit J1B 081 and Initiated Transfer Receive J1B 080 must be grounded If these discretes are not grounded then the initiated transfer discretes shall determine the mode usually with external switches connected to these inputs 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont A429 LRN 3 Configuration 3 Discretes A429 LRN 3 Configuration Config 31 Config 30 Config 29 Spare Low Speed IRS High Speed Omega Low Speed Spare High Speed GPS Low Speed GPS High Speed Spare High Speed Spare Low Speed RrRrRrOOO oO r3 L0 A429 LRN 3 Number 2 Discretes A429 LRN 3 Number Config 33 Config 32 LRN 0 0 LRN 1 0 LRN
182. inistrator s U S FAX No is 602 436 6317 X Local reproduction of this form is encouraged AldVLS LON OG NECESSARY IF MAILED IN THE UNITED STATES BUSINESS REPLY MAIL FIRST CLASS PERMIT NO 3532 PHOENIX AZ POSTAGE WILL BE PAID BY ADDRESSEE a E zi oS HONEYWELL INC PHOENIX ARIZONA 85036 9975 ATTN CUSTOMER SUPPORT QUALITY ADMINISTRATOR 0 45434 STAPLE Qe Os Honeywell Please cut along the dotted line Please cut along the dotted line Qe oS FOR HONEYWELL USE ONLY REPORT OF POSSIBLE DATA ERROR Hoesen DATE RECEIVED To help us improve the quality of this publication Honeywell encourages any report of possible data error PUBLICATION INFORMATION Publication Volume No ATA Latest Issue Date Number Book or Number From Title Page Addendum Publication Document CMM SDI Other Title Type GEM a SMM READER INFORMATION Please check all that apply O Trainer O Technician O Librarian O Engineer O Other specify Your Name optional Company Name City State Province Zip Code Country Telephone Number FAX Number POSSIBLE DATA ERROR Paragraph Description of Possible Data Error HONEYWELL REPLY Street Address Please mail or FAX completed form to Customer Support Quality Administrator If returning by mail please tape closed U S postal regulations prohibit the use of sta
183. ions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX Reinstallation of the mounting tray for the IRU requires the following e Leveling Device Honeywell Part No UG5046 e Four sets of shim washers 0 250 6 35 mm to 0 375 in 9 52 mm I D and 0 750 in 19 05 mm to 0 875 in 22 22 mm O D containing the following Qty 2 at 0 100 in 2 54 mm thick Qty 2 at 0 050 in 1 27 mm thick Qty 4 at 0 015 in 0 381 mm thick Qty 4 at 0 006 in 0 152 mm thick No additional special equipment or materials other than those commonly used in the shop are required for reinstalling units in existing trays and clamps and adjusting the system Do not over tighten mounting screws Where torque values are not given finger tightening of the mounting screws is acceptable Procedure for the AT 300 Radio Altimeter Antenna A Removal and Reinstallation Procedures 1 Remove antenna a Loosen remove and set aside four No 10 pan head screws b Unseal and remove antenna c Disconnect cable connectors 2 Reinstall antenna CAUTION THE RADIO ALTIMETER MUST BE ORIENTED POLARIZED TO MINIMIZE ANTENNA TO ANTENNA LEAKAGE AT 300 ANTENNAS HAVE A SMALL ARROW PAINTED ON THE FACE THESE ANTENNAS MUST BE MOUNTED SO THAT THE ARROWS POINT TO THE AIRCRAFT CENTERLINE AS SHOWN IN FIGURE 4 1 a Clean the mounting surface well with emery cloth to provide a good ground between the aircraft and antennas
184. is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 Function Connector Pin Connects To ITT AL 137J1B 1 ITT CH 2 3 WING FUEL QTY 4 WING FUEL QTY 25 N1 SPEED N1 SPEED FUEL FLOW DRUM FUEL FLOW COMMON FUEL FLOW IMPELLER FUEL HTR TEMP EXC FUEL HTR TEMP EXC FUEL HEATER TEMP FUEL HEATER TEMP C OIL PRESSURE C OIL PRESSURE TEMP EXC TEMP EXC TEMP TEMP OIL OIL OIL OIL STABILIZER POSITION STABILIZER POSITION STABILIZER POSITION AILERON POSITION AILERON POSITION ATLERON POSITION 137J1B 33 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 Function Connector Pin Connects To ELEVATOR POSITION H 137J1B 34 ELEVATOR POSITION W 35 ELEVATOR POSITION L 36 23 7 N2 SPEED 38 C N2 SPEED 39 DEEC OUTPUT 40 ARINC 429 CH A 41 L DEEC INPUT 42 ARINC 429 43 C VIBRATION INPUT 44 ARINC 429 45 R DEEC INPUT 46 ARINC 429 47 FUEL COMPUTER INPUT 48 ARINC 429 49 GPWS OUTPUT 50 ARINC 429 CH A 51 52 RESERVED FDR OUT 53 ARINC 573 717 FIGURE
185. isengage the Dzus fasteners on the unit b Slide unit out of panel c Disconnect cable connectors 2 Reinstall GC 810 Flight Guidance Controller a Mate cable connectors with unit connectors and slide unit into panel b Engage the Dzus fasteners on the unit B Adjustment Procedures Not Applicable C Repair Procedures 1 Replacement of the Pushbutton Switch Lamps CAUTION BE CAREFUL TO AVOID CRACKING THE PLASTIC SWITCH PUSHBUTTON WHEN PERFORMING STEP 11 C 1 a NOTE Access to these lamps does not require removing the controller from the instrument panel a Use an IC puller and insert the tips into the notch at the top and bottom or on each side of the switch pushbutton Gently pull straight out until the pushbutton assembly moves out from the switch housing b Grasp the pushbutton assembly and slide it out until it reaches its stop and then let the pushbutton assembly hinge down c Remove and replace the defective lamp d Hinge the pushbutton assembly up and slide the assembly back into the housing until it locks into position 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 2 Replacement of the IAS MACH Knobs and PUSH CHG Pushbutton NOTE The pushbutton setscrews are reached through access holes in the outer knob Rotate the outer knob fully CCW Use a 0 048 inch O D
186. lar level for use in the next step Return the airplane to its original level position Check the position of the bubble in the tubular level It should be within one division of the position in step 18 B 2 d Check the position of the bubble in the circular level It should still be within the second ring If the position of the bubble in the tubular level has moved more than one division repeat steps 18 B 2 d and e If repeating steps d and e is not successful the entire leveling procedure must be repeated When step 18 B 2 e is successful torque the four mounting bolts to 25 inch pounds 5 inch pounds Check that the bubble in the circular level is within the second ring and note the position of the bubble in the tubular level Pitch the airplane the same amount that was used in step 18 B 2 d and note that the bubble in the tubular level did not move more than one division Return the airplane to level remove the leveling fixture and install the IRU in the mounting tray in accordance with paragraph 15 A 2 C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 19 Procedure for the Mode Select Unit MSU A Removal and Reinstallation Procedures 1 Remove MSU a Disengage the Dzus fasteners on the unit b Slide the unit out of the aircraft mounting l
187. le 3 1 Interconnect Information cont DISPLAY UNIT NO 5 cont DU 870 Function Connector Pin Connects To DLS H C13001 28 24 S C131J1 29 DLS L AL ZAJAS 5 C131J1 42 GND ALS H 229 Gla enn 5 131 1 28 15 1 24 et ene ris 5 131 1 41 GND RESERVED RESERVED HDLC OUT RESERVED HDLC OUT BUS 3 TERM RESERVED BUS 2 FED BUS 2 NO TERM 1 DU VALID GND OPEN BUS 1 han BUS 1 NO TERM 1 REMOTE LT SENSOR GND SEE C130J1 28 SEE C130J1 29 RESERVED RESERVED BUS 4 TERM DU 5 PB5 STD C9J1 71 GND OPEN DU 5 PBA IN HPA 115J2 26 GND OPEN C115J2 26 RESERVED BUS 2 TERM 49 DU 5 PB3 METRIC 50 115J2 25 GND OPEN 115 2 25 DU 5 PB2 FORMAT 51 115J2 24 GND OPEN C115J2 24 BUS 1 TERM 52 REM LT SENSOR PWR H 53 REM LT SENSOR PWR L C130J1 54 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont DISPLAY UNIT NO 5 cont DU 870 Function RESERVED RESERVED RESERVED BUS 4 H BUS 4 NO TERM 1 DU 5 1 FPA GND OPEN WX BUS 2 TERM RESERVED KNOB PB COMMON WX BUS 1 TERM DU OVERTEMP GND OPEN DU WRAPAROUND H A 429 XMTR L RESERVED RESERVED WX BUS 3 WX BUS 3 RESERVED RESERVED RESERVED WX BUS 2 WX
188. le containing the circuit card assembly out of the enclosure 3 Using a pair of diagonal cutters cut the straps jumper wires in two places and remove the wire fragment Refer to SECTION 3 of this manual for a listing of the jumpers to be cut 4 After cutting all the required jumpers install the module in its enclosure and secure with the two captive screws 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX C Repair Procedures Not Applicable 15 Procedure for the Inertial Reference Unit IRU A Removal and Reinstallation Procedures CAUTION IF THE IRU MOUNTING TRAY IS MOVED IN ANY DIRECTION A COMPLETE TRAY ALIGNMENT MUST BE DONE REFER TO PROCEDURE IN PARAGRAPH 18 1 Remove IRU a Loosen the two thumb wheel clamps until they disconnect from the support hooks b Slide the unit out of the mounting tray 2 Reinstall IRU CAUTION WHEN PLACING THE UNIT ON THE MOUNTING TRAY DO NOT FORCE FIT IF MATING IS DIFFICULT REMOVE THE UNIT AND CHECK FOR CONNECTOR PINS THAT MAY BE BENT OR OUT OF ALIGNMENT ALSO VISUALLY CHECK THE ALIGNMENT OF THE RECEPTACLE ON THE MOUNTING TRAY a Place the unit on the mounting tray Slide it onto the three guide pins Slide the unit backwards until its connectors are fully engaged with the mating connectors of the mounting tray b Secure the unit
189. ment SYSTEM MAINTENANCE Honeywell MAINTE FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont Function IDENT RESISTOR R3 IDENT RESISTOR COM RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED ASCB NO 2 PRI H ASCB NO 2 PRI L RESERVED RESERVED RESERVED RESERVED IDENT RESISTOR R4 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED LASEREF III Connector Pin Connects To C170J1A C1 C2 FIGURE 8 1 GND L GND SEE C170J1A C10 D14 C170J1A D15 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 BP SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INERTIAL REFERENCE UNIT NO 2 cont LASEREF III Function Connector Pin Connects To LAB LOCKOUT C170J1A E1 GNSSU NO 2 2 A 429 RCVR FIGURE 8 2 GNSSU NO S T S A 429 RCVR 5 FIGURE 8 2 CTVAL1 E6 CTVAL2 E7 RESERVED E8 RESERVED 9 FAIL LOGIC E10 AC TO BATT XFER E11 RESERVED E12 RESERVED E13 RESERVED E14 RESERVED E15 RESERVED F1 RESERVED F2 RESERVED F3 GNSSU 2 TIME MARK 1 H F4 T S Cl49J1 19 GNSSU 2 TIME MARK 1 L F5 S T m C149J1 20 ND RESERVED RESERVED RESERVED RESERVED ASCB NO 1 PRI H
190. n cont DISPLAY UNIT NO 3 cont DU 870 10 BP Function Connector Pin Connects To 1 SIGNAL GROUND SIGNAL GND RESERVED RESERVED 1 WX BUS 3 TERM RESERVED SPARE SPARE PORT SEL 3 GND OPEN 135J1 43 E135J1 18 PORT SEL 2 GND OPEN E135J1 15 PORT SEL 1 GND OPEN I D 3 GND OPEN 0 I D 2 GND OPEN SIGNAL GND I D 1 GND OPEN 2 RESERVED CHASSIS GND RESERVED RESERVED RESERVED RESERVED SOFTWARE ENABLE GND OPEN SOFTWARE ENABLE 100 GND OPEN 28 VDC POWER 101 28 VDC POWER 102 FIGURE 8 6 28 VDC POWER 103 28 VDC POWER RETURN 104 28 VDC POWER RETURN 105 28 VDC POWER RETURN 132J1 106 DC POWER GND 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont REVERSIONARY CONTROLLER NO 1 RC 820 Function Connector Pi Connects To PILOT PFD 135 1 1 13031 1 BRIGHTNESS POT 1 PILOT MFD 4 BRIGHTNESS POT PILOT PFD ON GND OPEN 7 PILOT PFD OFF GND OPEN 8 130J1 22 PILOT PFD OFF GND OPEN x9 C190J1C 31 PILOT PFD OFF GND OPEN 10 E190J1C 31 PILOT PFD OFF GND OPEN 11 190J1C 31 AUTO EICAS REV 3 GND OPEN 12 C135J1 17 E135J1 13 AUTO EICAS REV 1 GND OPEN 13 C135J1 15 E135J1 16 AUTO EICAS REV 2 GND OPEN 14 C135J1 16 E135J1 23 EICAS SG SEL 2 GND OPEN 15 C135J1 13 E135J1 17
191. nt The maximum cable length for an IAC DU display bus from an IAC to its termination is 200 feet There shall be a minimum of 23 inches of cable between adjacent stubs ref Figure 6 1 and 6 3 The preferred method of constructing a DU stub connection is the same as for the ASCB stub ref Figure 5 2 Using this method the unshielded stub length can be up to 6 inches Butt splices with solder rings will be utilized for all stub interconnections ref Figure 5 2 The bus shield connections at each stub shall be accomplished with a butt splice which will provide a maximum shield to shield connection of 0 3 inches If a stub shield is used connect the stub shield to the bus shield with a butt splice of minimum length less than 2 inches 20 AWG wire All exposed wires at the splice and wires used to connect shields at the splice shall be covered with an overbraid material The overbraid material shall then be tied to the shield or airframe ground The bus shields shall be grounded to the airframe ground at each LRU connector with a minimum length 20 AWG wire Refer to paragraph 4 1 3 4 for proper shield grounding points and overbraid or backshell protection There shall be no unshielded portion of the IAC DU buses Shields should be bonded to the outer shell of each LRU It is very important that the IAC DU buses in a redundant system be installed with consideration for damage failure modes Therefore the buses should be bundled separat
192. ocation and disconnect the cable connector s 2 Reinstall MSU a Mate the cable connector s with the unit connector s and slide the unit into the aircraft mounting location b Engage the Dzus fasteners on the unit B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 20 Procedure for the RC 820 Reversionary Controller A Removal and Reinstallation Procedures 1 Remove RC 820 Reversionary Controller a Disengage the Dzus fasteners on the unit b Slide the unit out of the aircraft mounting location and disconnect the cable connector 2 Reinstall RC 820 Reversionary Controller a Mate the cable connector with the unit connector and slide the unit into the aircraft mounting location b Engage the Dzus fasteners on the unit B Adjustment Procedures Not Applicable C Repair Procedures 1 Replacement of the SG Knob and PUSH TEST Pushbutton NOTE The pushbutton setscrews are reached through access holes in the outer knob a Rotate the outer knob to the NORM position b Use a 0 048 inch O D 6 flute Bristol wrench to loosen the setscrews in the outer knob c Rotate outer knob until access hole lines up with setscrews on inner PUSH TEST pushbutton and loosen two setscrews d Slide the knob and
193. off of the shaft Page 4 9 Sep 1 1996 22 05 21 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX e On new knob and pushbutton make sure that the setscrews are out far enough to allow knobs to slide onto shaft Apply retaining compound to setscrews f Slide the outer knob onto the shaft Do not tighten setscrews g Slide the PUSH DCT pushbutton onto the shaft h Align the access holes in the outer knob with the setscrews in the PUSH DCT pushbutton i Ensure the PUSH DCT lettering is straight and tighten the PUSH DCT pushbutton setscrews j Ensure that the space between the knob and the front panel is approximately 0 030 inch 0 8 mm K Tighten the knob setscrews I Visually check the spacing between the knob and front panel to ensure that the knob has not slipped during installation 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell ji FALCON 900EX 9 Procedure for the DL 900 Data Loader A Removal and Reinstallation Procedures 1 Remove DL 900 Data Loader a Disengage the Dzus fasteners on the unit b Slide the unit out of the aircraft mounting location and disconnect the cable connector s 2 Reinstall DL 900 Data Loader a Mate the cable connector s with the unit connector s
194. oles in the outer knob with the setscrews in the PUSH SYNC pushbutton Ensure PUSH SYNC lettering is straight and tighten the PUSH SYNC pushbutton setscrews Ensure that the space between the two knobs is approximately 0 030 inch 0 8 mm Tighten the knob setscrews Visually check the spacing between the knob and front panel to ensure that the knob has not slipped during installation 2 Replacement of the BRG Knob With knob in OFF position loosen the setscrews with a 0 048 inch O D 6 flute Bristol wrench Slide the knob off of the shaft On new knob make sure that the setscrews are out far enough to allow knob to slide onto the shaft Apply retaining compound to setscrews Slide the knob onto the shaft Ensure that the space between the knob and the front panel is approximately 0 030 inch 0 8 mm Tighten the knob setscrews Visually check the spacing between the knob and front panel to ensure that the knob has not slipped during installation 3 Replacement of the CRS Knob and PUSH DCT Pushbutton NOTE The pushbutton setscrews are reached through access holes in a b the outer knob Rotate the outer knob fully CCW Use a 0 060 inch O D 6 flute Bristol wrench to loosen the setscrews in the outer knob Rotate outer knob until access hole lines up with setscrews on inner PUSH DCT pushbutton and loosen two setscrews Use a 0 048 inch O D 6 flute Bristol wrench Slide the knob and pushbutton
195. ont DATA ACQUISITION UNIT DAU NO 2 cont DA 800 wre Function Connector Pi Connects To CTR DEEC MANUAL 6 0 137J2A 1 CTR FUEL FLTR BYPASS G 0 2 LT WING FUEL LVL LOW 0 0 3 RT WING FUEL LVL LOW G 0 4 LT WING LOW FUEL 0 0 5 RT WING LOW FUEL G 0 6 FUEL XFR VALVE OPEN G 0 7 FUEL XFR MSG AMB GRN G 0 8 CTR ENG ANTI ICE ON G 0 9 CTR BLEED OVERHEAT G 0 10 CREW A C OVERHEAT G 0 11 RT PITOT HEAT OFF 0 0 12 RT AOA HEAT OFF 06 0 213 WEIGHT ON LT MN GEAR 6 0 14 FIGURE 8 5 WEIGHT ON NOSE GEAR G 0 15 FIGURE 8 5 WEIGHT ON RT MN GEAR 9 0 16 FIGURE 8 5 THRUST REV LVR ARMED 6G 0 17 THRUST REV IN TRANSIT 9 0 18 THRUST REV DEPLOYED G 0 19 WHEEL BRAKE ACTIVE 06 0 20 PARKING BRAKE SET G 0 21 FWD SERVICE DOOR OPEN G 0 22 IN FLT BAGG DOOR OPEN G 0 23 MASTER CAUTION ANN G 0 COPILOT PUSH TO TALK G 0 FDR FAIL G 0 EXT SLATS EXTENDED G 0 INBRD SLATS EXTENDED G 0 MED AIR BRKS RETRACT G 0 INT AIR BRKE RETRACT G 0 CTR HYD PRESSURE LOW G 0 HF 2 SELCAL ACTIVE G 0 SPARE G 0 SPARE G 0 SPARE G 0 35 SPARE 0 0 137J2A 36 as Ba Baas Baa Baan aa B aa Baa B aaa Baa aaa
196. or BOTH depending on what data is to be transferred NOTE f the optional third FMS is not installed do not perform step 13 B 3 c If a third FMS is installed perform step 13 B 3 c before performing step d On the NAV MAINTENANCE page select a dual configuration of the FMS i e FMS 1 to FMS 3 or FMS 2 to FMS 3 Perform step 13 B 3 d and substitute FMS 3 for FMS 1 or 2 depending on the dual configuration selected On the TRANSFER OF CUSTOM DB or NAV DB page select TO FMS 2 or FR FMS 2 depending on whether you are transferring data from FMS 1 IAC 1 to FMS 2 IAC 2 or from FMS 2 IAC 2 to FMS 1 IAC 1 respectively NOTE It is important that the direction of transfer be correct The affected database in the receiving IAC is erased and lost when the transfer begins On the CONFIRM TRANSFER OF CUSTOM DB or NAV DB page confirm selection by selecting YES or NO Monitor 96 of loading progress When complete the message DB TRANSFER COMPLETE is displayed The IAC FMS does a restart NOTE The data load process must be repeated from the beginning when power is interrupted ABORT is selected or other problems that stop the loading process occur 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 4 Transferring the Checklist From or To the IAC Connect the IAC to PC adapter harness to the
197. or backshell protection There shall be no unshielded portion of the WX DU buses Shields should be bonded to the outer shell of each LRU 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont ELECTRICAL INTERCONNECT DEFINITION This paragraph provides the electrical interconnect definition for the integrated avionics system defined by M1558 1563 The interconnect information is ordered per unit connector designation numbers 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont MICRO AIR DATA COMPUTER MADC NO 0 Function 100 101 102 103 104 UNIT UNIT UNIT UNIT UNIT GND OPEN 9J1 1 GND OPEN 2 GND OPEN 53 GND OPEN GND OPEN 5 UNIT ID5 GND OPEN 6 UNIT ID6 GND OPEN 7 SDI 1 GND OPEN 8 SDI 2 GND OPEN 9 501 3 GND OPEN 10 SPARE 11 WOW GND OPEN SIGNAL GROUND SPARE SPARE SPARE 12 13 14 GND OPEN GND OPEN GND OPEN GND OPEN 28 V OPEN 28 V OPEN KNOTS GND OPEN KNOTS GND OPEN KNOTS GND OPEN KNOTS GND OPEN KNOTS GND OPEN 28 VDC POWER 28 VDC POWER RETURN OVERSPEED WARNING DIS
198. ot exceed eight inches It should be noted that the screening scheme that is followed throughout this installation bulletin was devised to achieve the best protection against a lightning strike or HIRF However in order to achieve the best screening against EMI it is recommended that the shield of twisted wires is grounded at the transmitting end The preferred method is no daisy chaining If daisy chaining is required please review the segregation of the system shields prior to daisy chaining A 20 gauge wiring should be used for tying shields to ground All DC power grounds shall be tied together all signal grounds shall be tied together and all lighting grounds shall be tied together DC power signal and lighting ground groups are then tied together at a single point and connected to the airframe The aircraft grounding diagram on the next page illustrates this grounding method It is very important that this grounding technique be adhered to Do not tie the various ground wires to multiple aircraft frame points and depend on the aircraft structure itself to provide a low impedance path for the individual grounds ONLY chassis grounds and shield grounds are grounded at multiple points in the aircraft 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information
199. page of this document SYSTEM Honeywell FALCON 900EX 2 Transferring the Custom Database To or From the DL 900 Data Loader The custom database can be transferred to or from the data loader When loading the custom database from the data loader the custom database is completely replaced by the contents of the disc including stored flight plans and pilot defined waypoints When transferring the custom database to a disc both the pilot defined waypoints and flight plans are transferred This option keeps a permanent record of the custom database for loading in case of IAC replacement or other losses of the custom database Refer to the following steps to transfer the custom database a If the DL 900 Data Loader is not installed in the aircraft connect the data loader cable to the aircraft connector Apply power to the data loader using the appropriate aircraft circuit breaker Push POWER switch on data loader The POWER LED shall light and after the powerup BITE sequence is completed the DATA LED shall light On data loader select LEFT or RIGHT or if the third FMS is installed select AUX If transferring from the data loader to the IAC insert custom data base disc in data loader If transferring from the IAC to the data loader insert a formatted disc If a disc needs formatting use the MAINTENANCE page option On the CD 810 Control Display Unit CDU select the DATA LOAD page from the NAV INDEX page 2 On t
200. play indication on the PFD C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 23 Procedure for the SM 200 Servo Drive and the SB 201 Drum and Bracket Assembly A Removal and Reinstallation Procedures 1 Remove SM 200 a Disconnect cable connector from servo drive b Cut safety wire and remove four screws securing servo drive to drum and bracket assembly c Slide servo drive out of drum and bracket assembly 2 Reinstall SM 200 a Slide servo drive into rear of drum and bracket assembly and secure with four screws Honeywell Part No 4011086 Safety wire all four screws with Low Mu Monel wire 0 020 inch diameter b Mate servo drive connector with cable connector 3 Remove SB 201 a Remove servo drive in accordance with paragraph 23 A 1 b Release bridle cable tension c Cut safety wire on four screws securing retaining plate and remove and set aside screws and retaining plate d Remove and set aside four cable keepers Honeywell Part No 2518330 e Cut safety wire and remove and set aside two screws securing swaged cable terminals to drum f Unwrap bridle cables from drum g Remove and set aside four nuts bolts and washers securing drum and bracket assembly to airframe h Lift drum and bracket assembly away from airframe 4
201. ples If sending by FAX the Quality Administrator s U S FAX No is 602 436 6317 Local reproduction of this form is encouraged AldVLS LON OG NECESSARY IF MAILED IN THE UNITED STATES BUSINESS REPLY MAIL FIRST CLASS PERMIT NO 3532 PHOENIX AZ POSTAGE WILL BE PAID BY ADDRESSEE a E zi oS HONEYWELL INC PHOENIX ARIZONA 85036 9975 ATTN CUSTOMER SUPPORT QUALITY ADMINISTRATOR 0 45434 STAPLE SYSTEM Honeywell FALCON 900EX RECORD OF REVISIONS VOLUME II Upon receipt of a revision insert the latest revised pages and dispose of superseded pages Enter revision number and date insertion date and the incorporator s initials on the Record of Revisions The typed initials HI are used when Honeywell Inc is the incorporator Revision Revision Insertion Revision Revision Insertion Number Date Date By Number Date Date By 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Blank Page 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX LIST OF EFFECTIVE PAGES VOLUME II Original 0 Sep 1 1996 SUBHEADING AND PAGE REVISION SUBHEADING AND PAGE REVISION Title 3 29 T 1 0 3 30 T
202. plicable instructions for replacing lamps knobs and set screws are included Adjustment information is called out as required CAUTIONS 1 SHOULD ANY INSTALLATION CRITICAL CASES ARISE WITH THE REINSTALLATION OF ANY UNIT YOU MUST COMPLY 100 PERCENT WITH THE INSTRUCTION 2 TO PREVENT DAMAGE TO EQUIPMENT TURN AIRCRAFT POWER OFF WHEN REMOVING OR INSTALLING LRUs Equipment and Materials NOTE Refer to the applicable leading particulars table in SECTION 2 of this manual for replacement gaskets lamps knobs and set screw part numbers Maintenance materials that are identified with Honeywell Material Number HMN are as follows 97D0878 HAZARD CODE 210D Retaining compound Loctite Assure No 425 surface curing threadlocker Loctite Corp Newington CT 97P5778 HAZARD CODE 110D Adhesive sealant high strength noncorrosive RTV silicone MIL A 46146 Type III No DC 3145 translucent RTV Dow Corning Corp Midland NOTE Equivalent alternatives are permitted for the materials in this HMN list When replacing lamps in the GC 810 Flight Guidance Controller and a switch pushbutton puller is needed use an IC puller Augat Part No T 114 1 Uploading Downloading of the checklist files requires the following IBM compatible laptop personal computer PC IAC to PC adapter cable assembly Dassault Part No TBD 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrict
203. pushbutton off of the shaft e On new knob and pushbutton make sure that the setscrews are out far enough to allow knobs to slide onto shaft Apply retaining compound to setscrews f Slide the outer knob onto the shaft Do not tighten setscrews g Slide the PUSH TEST pushbutton onto the shaft h Align the access holes in the outer knob with the setscrews in the PUSH TEST pushbutton i Tighten the PUSH TEST pushbutton setscrews 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX j Ensure that the space between the knob and the front panel is approximately 0 030 inch 0 8 mm k Tighten the knob setscrews I Visually check the spacing between the knob and front panel to ensure that the knob has not slipped during installation 2 Replacement of the BRT and OFF REV Knobs a Rotate inner and outer knobs to OFF position b Use a 0 048 inch O D 6 flute Bristol wrench to loosen the setscrews c Slide the knobs off of the shaft d On new knob make sure that the setscrews are out far enough to allow the knob to slide onto the shaft Apply retaining compound to setscrews e Slide the outer knob onto the shaft ensuring that the line aligns with the OFF REV position f Ensure that space between knob and front panel is approximately 0 030 inch 0 8 mm g Tighten the knob setscr
204. r 4 47 27 Procedure for the WU 870 Antenna and Receiver Transmitter Unit 4 48 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX TABLE OF CONTENTS SECTION 4 Cont List of Illustrations FIGURE TITLE PAGE Figure 4 1 AT 300 Radio Altimeter Antenna Orientation 4 3 Figure 4 2 IC 800 IAC Test Connector Harness 4 23 Figure 4 3 IRU Mounting Tray Fan Housing 4 27 Figure 4 4 AHRU IRU Leveling Fixture 4 32 Figure 4 5 RT 300 Zero Adjustment Cable 4 40 Figure 4 6 SM 725 Actuator Complete Assembly 4 44 List of Tables TABLE TITLE PAGE Table 4 1 Degree Radian Conversion 4 31 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX SECTION 4 MAINTENANCE PRACTICES General This section provides instructions for removing reinstalling and adjusting each line replaceable unit LRU of the PRIMUS 2000 Integrated Avionics System that has been previously installed by the aircraft manufacturer or completion center Where ap
205. r disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Blank Page 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Table 3 1 Interconnect Information TABLE OF CONTENTS Title Deleted Deleted Deleted ELECTRICAL INSTALLATION AVIONICS STANDARD COMMUNICATION BUS DISPLAY BUS INTERFACE REQUIREMENTS ELECTRICAL INTERCONNECT DEFINITION SUPPLEMENTARY WIRING INFORMATION FIGURES APPENDIX CONFIGURATION MODULE DISCRETES FOR THE FALCON 900EX 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont LIST OF FIGURES Title Shield Grounding Philosophy ASCB Bus Construction ASCB Stub Construction IAC DU Bus Interface Unterminated DU DU Display Bus Termination Provision IAC DU Bus Interface Terminated DU WX DU Bus Interface Unterminated DU DU Picture Bus Termination Provision WX DU Bus Interface Terminated DU ASCB Connections Bus 1 Primary amp Bus 1 Backup ASCB Connections Bus 2 Primary amp Bus 2 Backup ARINC 429 Interfaces ARINC 429 Interfaces ARINC 429 Interfaces ARINC 429 Interfaces ARINC 429 In
206. r subsystems of the avionics system defined by M1558 1563 The ASCB consists of four multipoint serial synchronous digital communications networks two primary buses and two on side BACKUP BU buses Each bus is electrically isolated from the other buses The ASCB bus layout is shown in Figure 8 1 The ASCB complies with RTCA Document D0 160C which requires that the following installation requirements must be met There are four independent ASCBs denoted 1 PRI 2 PRI 1 BU and 2 BU each consisting of one shielded wire pair The ASCB transmission line shall have a characteristic impedance of 125 5 ohms The characteristic capacitance shall be 12 2 picofarads foot Filotex Part No 69654 Raychem 2524E0114 with thermorad jacket or equivalent can be used The ASCB transmission line shall be terminated at its two ends with noninductive 127 ohm resistors 1 1 2 watt metal film The minimum cable length between the last stub and the termination resistor shall be 23 inches Provide overbraid protection for exposed wires and resistors at the termination point The ASCB transmission lines shall have a maximum length between terminators of 125 feet There shall be a minimum of 23 inches of ASCB cable between adjacent stubs ref Figure 5 1 This is necessary to minimize reflections The preferred method of constructing a stub connection is shown in Figure 5 2 Using this method the total unshielded stub length can be up to 6 inc
207. rconnect Information cont APPENDIX A CONFIGURATION MODULE DISCRETES FOR THE FALCON 900EX 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont APPENDIX A CONFIGURATION MODULE DISCRETES FOR THE FALCON 900EX The configuration discretes shall be serialized into the IAC in twelve consecutive bytes These discretes shall be read by the I O CPU at power up and inserted into the swap RAM for the internal functions The configuration module shall use jumpers on a circuit card that define the configuration of the aircraft The following hardware implementation is in the configuration module Jumper installed Logic 0 Jumper removed Logic 1 CB Configuration Byte DISCRETE BYTE BIT GENERIC DESCRIPTION NOTES CB1 0 of AHRS IRSs F900EX allows 2 or 3 IRSs 1 1 of AHRS IRSs CB1 2 of ADCs 2 F900EX always has 2 MADCs CB1 3 of ADCs 1 CB1 4 of EFIS FWCs F900EX always has 3 EFIS FWCs CB1 5 of EFIS FWCs CB1 6 LSS Installed LSS is optional on F900EX 1 7 0 CB2 0 FGC Not Installed in this IACs 1 and 2 have autopilots IAC IAC 3 does not CB2 1 FMS Not Installed in this All combinations allowed IAC CB2 2 of FMSs 2 All combinations allowed CB2 3 of FMSs 1 CB2 4 SPARE CB2 5 SPARE CB2 6 SPARE CB2 7 1 CB3 0 A429 LRN1 Config All combinations allow
208. re 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell FALCON 900EX 14 Procedure for the IM 803 Installation Module NOTE The IM 803 defines the configuration of the aircraft in which the IAC is installed and is located on the side of the IAC A Removal and Reinstallation Procedures 1 Remove IM 803 a Loosen the two captive screws that attach the module to the enclosure b Grasp the handle and slide the module out of the enclosure 2 Reinstall IM 803 CAUTION IF THE IM 803 IS REMOVED FROM THE AIRCRAFT AND REPLACED WITH AN IM 803 FROM CUSTOMER OWNED SHELF STOCK OR WAS OBTAINED FROM DASSAULT OR HONEYWELL THE CONFIGURATION STRAPS WILL HAVE TO BE CUT IN ACCORDANCE WITH THE LIST IN SECTION 3 AND THE PROCEDURE IN PARAGRAPH 14 B OF THIS MANUAL a Carefully slide the module into the enclosure b Tighten the two captive screws B Adjustment Procedure Cutting Configuration Straps CAUTIONS 1 BE VERY CAREFUL WHEN CUTTING CONFIGURATION STRAPS SO AS NOT TO DAMAGE THE CIRCUIT CARD ASSEMBLY 2 PERFORM STRAP CUTTING IN AN ELECTROSTATICALLY SAFE ENVIRONMENT TO PREVENT DAMAGE TO THE CIRCUIT CARD ASSEMBLY 3 ALWAYS TRANSPORT THE CIRCUIT CARD ASSEMBLY IN ITS ENCLOSURE OR IN AN ANTISTATIC BAG 1 Loosen the two captive screws that attach the module to the enclosure 2 Grasp the handle and slide the modu
209. re an insurance value on the bill of lading Honeywell is self insured 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Test Equipment Specialized test equipment is not required for normal flight line maintenance of Honeywell avionics Certain standard commercially available avionics aids such as ramp signal checkers oscilloscopes meters etc may be useful for more detailed troubleshooting A breakout box can also be helpful for certain equipment and availability of this item can be discussed with a Honeywell Customer Engineer Customer Engineering A key element in Honeywell s corporate operations support is our worldwide customer engineering organization The members of this group are strategically located around the world These individuals have earned an excellent reputation within the avionics industry as the result of their high level of education experience dedication and responsiveness Customer engineering is ready to provide corporate operators with on site technical assistance provisioning consultation training and regulatory agency coordination In addition customer engineers will provide engineering interface assistance for other interrelated equipment on the aircraft and will support your maintenance engineers and technicians Continuing assistance is provided through telephone consult
210. refer to Honeywell s Corporate Operators Customer Support and Sales Directory Pub No 60 7390 17 A North America Central Support Center Honeywell Inc 1830 Industrial Ave Wichita KS 67216 Tel 316 522 8172 Fax 816 522 2693 Dallas Support Center Honeywell Inc 7825 Ridgepoint Drive Irving TX 75063 Tel 214 402 4300 Fax 214 402 4999 Ohio Support Center Honeywell Inc 8370 Dow Circle Strongsville OH 44136 Tel 216 243 8877 Fax 216 243 1954 Northwest Support Center Honeywell Inc 4150 Lind Ave Southwest Renton WA 98055 Tel 206 251 9511 Fax 206 251 9368 SPEX Administration Office Honeywell Inc 5353 West Bell Road Glendale AZ 85308 Tel 602 436 8961 Fax 602 436 7350 Canada Support Center Honeywell Ltd Aerospace Division 3 Hamilton Ave Ottawa Ontario Kly 4J4 Canada Tel 613 728 4681 Fax 613 728 7084 24 Hour Service CANADA 1 800 267 9947 U S A 1 800 USA SPEX Page 6 6 Sep 1 1996 22 05 21 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX International France Support Center United Kingdom Support Center Honeywell Aerospace Honeywell Avionics Systems Ltd 1 Rue Marcel Doret BP14 Edison Road 31701 Blagnac France Basingstoke Hampshire RG21 2QD Tel 33 6212 1500 England Fax 33 6130 0258 Tel 44 1256 51111 Fax 4
211. rental during the initial repair of the failed unit 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Warranty Statement Honeywell warrants that any article provided under the SPEX program will at the time of delivery conform to all applicable specifications and drawings and be free of defects in material and workmanship Honeywell s obligation under this warranty however shall be limited to repair of or at Honeywell s option replacement of any article which is returned to Honeywell within the stipulated twelve month warranty period For further information regarding exchange or rental units contact any of the Honeywell facilities listed at the end of this section or refer to Honeywell Pub No A65 8200 001 Exchange and Rental Ordering 1 Telephone Numbers Place an order by calling one of the following numbers UNITED STATES DALLAS TX 1 800 872 7739 214 402 4300 CANADA OTTAWA ONT 1 800 267 9947 UNITED KINGDOM BASINGSTOKE 44 1256 51111 FRANCE TOULOUSE ni nni aea ee 33 6171 9662 GERMANY GAUTING 49 89 89317 226 After normal working hours 49 89 850 3695 SINGAPORE ue eS M E EEG 65 542 1313 AUSTRALIA TULLAMARINE 61 3 330 1411 BRAZIL S O PAU
212. rs and slide the unit out of the tray c Stow the locking lever by pressing it up and into the slot in the handle until the latching button clicks into place 2 Reinstall DA 800 DAU a Press up on the inside at the top of the front handle to release the locking lever Move the locking lever out and down to release the locking cam CAUTION WHEN PLACING THE UNIT ON THE MOUNTING TRAY DO NOT FORCE FIT IF MATING IS DIFFICULT REMOVE THE UNIT AND CHECK FOR CONNECTOR PINS THAT MAY BE BENT OR OUT OF ALIGNMENT ALSO VISUALLY CHECK THE ALIGNMENT OF THE RECEPTACLE ON THE MOUNTING TRAY b Place the unit on the mounting tray Slide the unit backwards until its connectors are fully engaged with the mating connectors of the mounting tray c Making sure that the locking cam mates properly with the cam receptacle move the locking lever up and into the slot in the handle until the locking button clicks into place B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 8 Procedure for the DC 840 Display Controller A Removal and Reinstallation Procedures 1 Remove DC 840 Display Controller a b Disengage the Dzus fasteners on the unit Slide the unit out of the aircraft mounting location and disconnect the cable
213. rs to provide input to the customer satisfaction survey below We welcome all comments and recommendations PUBLICATION INFORMATION Volume No Book or Addendum Publication Document CMM SDI Other Title Type o GEM SMM Latest Issue Date From Title Page Publication Number READER INFORMATION Please check all that apply O Trainer Technician Librarian O Engineer O Other specify Your Name optional Company Name City State Province Zip Code Country Telephone Number FAX Number CUSTOMER SATISFACTION SURVEY Street Address Please check the YES or NO box to answer the following questions Yes No 1 Is the Publication technically accurate 2 Is information easy to find 3 15 information complete 4 Are figures easy to use 5 tables easy to use 6 Is the Publication used for training 7 Do you or your organization wish to remain on distribution for this Publication Excellent Good Poor Please rate this Publication in comparison to other documents you use L1 L1 L1 Please provide comments recommendations and or improvements that you would like to see in this publication Please mail or FAX completed form to Customer Support Quality Administrator If returning by mail please tape closed U S postal regulations prohibit the use of staples If sending by FAX the Quality Adm
214. s page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 IO BP Function Connector Pin Connects To I DU 5 WRAPAROUND H E190J1C 20 24 S T S 130 1 66 A 429 RCVR 13 190J1C 20 C190J1C 20 1 L 21 13001 79 190J1C 21 C190J1C 21 1 SPARE FGC DISC IN 22 GND OPEN 1 SPARE FGC DISC IN 23 GND OPEN SPARE L 24 A 429 RCVR 18 H 25 FIGURE 8 2 GND _ L GND 26 SEE E190J1C 13 SPARE CARD RESERVED 27 do E FIGURE 8 2 MLS 1 A 429 RCVR 4 EICAS LEFT SEL 30 E135J1 6 GND OPEN PFD 1 OFF GND OPEN 31 135J1 10 AURAL WARNING OUT 32 AURAL WARNING OUT B L 33 RSB RESERVED 34 RSB RESERVED 35 RSB SECONDARY H 36 RSB SECONDARY L 37 DISPLAY CONTROL 2 38 C115J1 7 190J1C 38 IOP RS 422 RX CL 39 S T 11991 8 L GND 190J1C FGC RESERVED 40 SPARE FGC DISC IN 41 28V 0PEN FGC RESERVED 42 FGC RESERVED 43 CROSS AP SENSE E190J1C 44 OUT 28 V OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 3 cont IC 800 Function Connector Pin Conn
215. s subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Blank Page 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document
216. set aside four nuts bolts and washers securing drum and bracket assembly to airframe g Disconnect cable connector and lift servo assembly away from airframe 2 Reinstall SM 810 Autothrottle Servo a Mount servo assembly rigidly to airframe with four 1 4 inch diameter bolts and four lock washers and nuts removed in paragraph 25 A 1 f b Connect aircraft cable connector to servo connector 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX INSTALLATION CRITICAL TO ENSURE CABLE TERMINAL CAPTURE USE ONLY 0 138 32 NC 2A STAINLESS STEEL DRILLED SCREWS HONEYWELL PART NO 2554911 1 STANDARD FILLISTER HEAD SCREWS MAY NOT PROPERLY RETAIN THE CABLE TERMINAL c Wrap bridle cables around servo drum Secure swaged cable terminals to servo drum with screws removed in paragraph 25 A 1 d or if a new servo use screws supplied with new servo Safety wire screws through adjacent holes in drum with Low Mu Monel wire 0 020 inch diameter and 4 inches long d Adjust control system and bridle cables to proper tension as instructed in the aircraft maintenance manual INSTALLATION CRITICAL TO ENSURE THAT THE CABLE CANNOT JAM BETWEEN THE DRUM AND KEEPERS THE DISTANCE BETWEEN THE KEEPERS AND DRUM SHALL BE MEASURED AFTER THE KEEPERS AND RETAINING PLATE ARE INSTALLED THE DISTANCE BETWEEN THE DRUM AND KEEPE
217. stem Sensor Unit GNSSU A Removal and Reinstallation Procedures 1 Remove GNSSU a Disconnect aircraft cable and antenna connectors b Remove and set aside four screws and washers securing GNSSU to airframe 2 Reinstall GNSSU a Secure the GNSSU to airframe using the four 10 32 screws lockwashers and flat washers that were removed and set aside b Mate unit connectors with appropriate antenna and cable connectors B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 13 Procedure for the IC 800 Integrated Avionics Computer IAC CAUTION IF AN IC 800 IS REMOVED FROM THE AIRCRAFT AND REPLACED WITH AN IC 800 FROM CUSTOMER OWNED SHELF STOCK OR WAS OBTAINED FROM DASSAULT OR HONEYWELL IT MAY BE NECESSARY TO DOWNLOAD THE CUSTOM AND NAVIGATION DATA BASE AND CHECKLIST FILES FROM THE MEMORY TO A 3 5 INCH DISKETTE BOTH THE NAVIGATION AND CUSTOM DATABASE AND THE CHECKLIST WILL NEED TO BE UPLOADED TO THE REPLACEMENT 1C 800 REFER TO PROCEDURES IN PARAGRAPH 13 B NOTES 1 The custom database is made up of flight plans and pilot defined waypoints This database can be loaded from a disc if available or cross loaded from one of the other IACs Please refer to your company s flight operations department for availability of custom
218. t SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont 149J1 GNSSU 1 ARINC 429 Interfaces Figure 8 2e 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 136J1B 28 V DC COMPUTER Le 2 Ds es AD 42189 R1 ARINC 429 Interfaces Figure 8 2f 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont 9J1 57 9J1 55 9J1 56 123J1 a 123J1 Z 123J1 V 136J1B 104 136J1B 105 136J1B 106 136J2B 104 136J2B 105 136J2B 106 149J1 2 149J1 3 SIGNAL GND 170J1A H10 170J1A H3 170J1A H4 170J1A H7 E170J1A H10 E170J1A H3 E170J1A H4 E170J1A H7 190J1B 106 190J1B 105 190J1B 104 190J1A 47 190J1A 48 190J1A 96 190J1D 81 190J1D 82 190J1D 80 190J1A 77 190J1A 6 190J1A 96 E190J1B 106 E190J1B 105 E190J1B 104 E190J1A 47 E190J1A 48 E190J1A 96 E190J1D 81 E190J1D 82 E190J1D 80 E190J1A 77 E190J1A 6 E190J1A 96 V V ASCB BUS 1 PRIMARY H ASCB BUS 1 PRIMARY L SEE FIGURE 8 1 ASCB BUS 1 BACKUP H AS
219. t Procedures Not Applicable C Repair Procedures Replacement of the Control Knobs NOTE Each knob has two 2 56 setscrews Use a 0 048 inch O D 6 flute Bristol wrench 1 Loosen the setscrews 2 Slide the knob off the shaft 3 On new knob make sure that the setscrews are out far enough to allow the knob to slide onto the shaft Apply retaining compound to setscrews 4 Slide the knob onto the shaft 5 Make sure that the space between the knob and the front panel is approximately 0 030 inch 0 8 mm 6 Tighten the setscrews 7 Visually check the spacing between the knob and the front panel to make sure that the knob has not slipped during installation 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 27 Procedure for the WU 870 Antenna and Receiver Transmitter Unit A Removal and Reinstallation Procedures 1 Remove WU 870 a Disconnect the cable connector from the unit b Remove and set aside the hardware securing the unit to the airframe 2 Reinstall WU 870 a Secure unit to airframe with applicable hardware b Mate the cable connector with the unit connector B Adjustment Procedures 1 Adjust WU 870 Antenna and Receiver Transmitter Unit on ground NOTE This procedure must be done by two persons One in the cockpit and one at the WU 870 WARNINGS
220. t each LRU connector with a minimum length 20 AWG wire Refer to paragraph 4 1 3 4 for proper shield grounding points and overbraid or backshell protection The DAU shall have an in line bus coupler connected between DAU channel B and the cross side BACKUP ASCB bus ref Figure 8 1 This bus coupler is used to isolate the cross side backup ASCB bus from a DAU failure It is very important that the ASCB buses be installed with consideration for damage failure modes Therefore the buses should be bundled separately wherever possible should not pass through common connectors or feedthroughs and should not be installed in high risk areas such as wing leading edges engine shrapnel path etc To ensure the required integrity of the ASCB System the ASCB bus paths shall be installed such that they would never all be exposed to water simultaneously This requirement is deemed INSTALLATION CRITICAL To ensure the required integrity of the ASCB System the ASCB bus cable shall use a waterproof jacket The jacket shall also resist caustic fluids which are likely to be found in aircraft and shall be flame resistant This requirement is deemed INSTALLATION CRITICAL To ensure the required integrity of the ASCB System all ASCB data buses shall not be passed through the same airframe connector They shall be separated by side on side in one connector off side in the other NOTE This requirement is not applicable to the actual LRU only adjacent pin
221. t each connector backshell 20 AWG pig tail of six inches maximum length will connect the group of shields to the LRU local earth post Twisted Shielded Pairs Unbalanced The shields of these signal cables will be grounded only at the signal source end of the cable by gathering the shields at each connector backshell 20 AWG pig tail of six inches maximum length will connect the group of shields to the LRU local earth post Twisted Shielded Triples The screens of these signal cables will be grounded for analog signals as in paragraph 4 1 3 4 1 and for digital signals as in paragraph 4 1 3 4 2 Audio Analog Signal Cable Screens The signal source cable end of these shields will be connected to spase ground they must not be grounded via connector backshells ALL WIRES SHOULD BE WIRED AS SHOWN ABOVE UNLESS OTHERWISE SHOWN WITHIN THIS TABLE 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont DATA BUS TO SPLICE BOX CONNECTION ANALOG SIGNAL ANALOG SIGNAL SOURCE ANALOG AUDIO SIGNAL SOURCE ANALOG SIGNAL SOURCE ARINC 429 ARINC 429 AND AND RS 422 BUSSES RS 422 BUSSES USE CONNECTOR BACKSHELL USE CONNECTOR BACKSHELL GROUNDING METHOD GROUNDING METHOD AD 19920 R1 Shield Grounding Philosophy Figure 4 1
222. tag attached to unit and any additional information if required 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX b Shipping Instructions 1 For North America Customers Ship via Federal Express Standard Air two day delivery If not served by Federal Express ship via airline direct airfreight not via a freight forwarder Shipment via a surface carrier may result in assessment of LATE RETURN CHARGES 2 For Europe and Africa Customers Return unit to the Honeywell Customer Support Center which issued the replacement or with prior arrangement to any one of the following addresses a Honeywell Avionics Systems Ltd c o Burlington Air Express Unitiair Centre Great South West Road Feltam Middlesex TW 14 8NT England U K b Honeywell Aerospace 1 Rue Marcel Doret 31700 Blagnac c o SCAC Air Service 6 Allee Henri Potez 31702 Blagnac 3 For Other International Customers Return unit to the Honeywell Customer Support Center which issued the replacement Shipments returning to the United States should be via Burlington Air Express If you are not served by Burlington Air Express ship via Emery Airfreight or by direct airline airfreight Consign shipments to Honeywell Inc c o F H Kaysing Co U S Customs House Broker Mid Continent Airport Wichita Kansas 67209 U S A NOTE Do not insure or decla
223. terconnect Information cont 4 9 9J1 72 SSEC DISABLE 1 vo OO C9J1 72 SSEC DISABLE 2 eT O 91 70 PILOT S MADC TEST SW AD Oo 0941 70 COPILOT S MADC TEST SW AD 41498 SSEC Disable and MADC Test Switch Diagram Figure 8 8 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 190J1A 88 C190J1A 88 190J1D 105 C190J1D 105 190J1C 8 C190J1C 8 190J1C 6 C190J1C 6 190J1D 100 C190J1D 100 28VDC PRIMARY BUSA SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont PILOT S TRIM SWITCHES COPILOT S TRIM SWITCHES DN ARM DNDRIVE TO AIRCRAFT UP DRIVE UP ARM EMER TRIM NOSE DOWN TO AIRPLANE EMERGENCY TRIM MOTOR EMER TRIM NOSE UP s AIRPLANE TAILPLANE CB CONTROL BOX GC INPUT SIGNAL POLARITY 28VDC EMER TRIM NOT ACTIVATED 111 32 OPEN EMER TRIM ACTIVATED AD 41499 Pitch Trim Interface Diagram Figure 8 9 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont Deleted Figure 8 10 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of t
224. terfaces ARINC 429 Interfaces RS 232 Test Connector Diagram IRS Strapping Weight on Wheels Switch Diagram Power Distribution Power Distribution Lighting Power Dimming Lamp Test SSEC Disable and MADC Test Switch Diagram Pitch Trim Interface Diagram THIS PAGE INTENTIONALLY LEFT BLANK Miscellaneous Switches Stick Shakers Single Radio Altimeter TAC DU WX Interfaces 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont LIST OF FIGURES cont Title Alt Alert AP Off VIA Horns and Check PFD Annunciators Pilot Event Marker LIST OF TABLES Title Connector Wire Gauge Limitations Circuit Breaker Selections 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 1 SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont Deleted Deleted Deleted ELECTRICAL INSTALLATION This paragraph covers the electrical installation of the M1558 1563 avionics system Paragraph 4 1 covers general installation requirements The specific installation requirements are covered in paragraph 4 2 and 4 3 General Requirements DC Power The aircraft DC power generator outputs must be 27 5 volts nominal The minimum and m
225. the circular level is 0 1 degree 6 arc minutes per graduation The sensitivity of the tubular levels is 20 arc seconds 0 0055 degree per graduation d The IRS Installation Software displays pitch roll and heading in radians As an aid Table 4 1 provides a degree radian conversion Table 4 1 Degree Radian Conversion Degree Radian 1 0000 degree 60 arc minutes 017453 radian 0 2000 degree 12 arc minutes 003491 radian 0 1000 degree 6 arc minutes 001745 radian 0 0055 degree 20 arc seconds 000096 radian 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX 20 ARC SECONDS 0 0055 DEG PER GRADUATION THROUGH TUBULAR LEVELS HOLE 0 1 DEGREE 6 ARC SECONDS PER GRADUATION CIRCULAR LEVEL AD 46557 Figure 4 4 AHRU IRU Leveling Fixture e Check the circular level of the leveling fixture The tubular levels are not used in this procedure Adjust the level of the mounting tray by installing shims as required to have the bubble in the circular level inside of the second ring refer to Figure 4 4 The mounting tray will be level to within 0 2 degrees with respect to the airframe f Torque the four mounting bolts to 25 inch pounds 5 inch pounds Check the circular level and verify that the bubble has not moved outside of the second ring The mounting tray will now be level
226. tion Connector Pin Connects To I SPARE DIO DISC IN C190J1B 84 GND OPEN 1 SPARE DIO DISC IN 85 GND OPEN 1 RESERVED CROSS SIDE 86 AWP MASTER GND OPEN 1 PILOT STICKSHAKER 87 FIGURE 8 12 28V 0PEN SPARE DIO DISC IN 88 28V 0PEN RSB RESET GND OPEN 89 DP2 RESET GND OPEN 90 RESERVED MASTER WARNING 91 HORN GND OPEN SPARE CARD RESERVED 92 SPARE CARD RESERVED 93 CONFIG MODULE 5V POWER 94 C199J1 1 CONFIG MODULE RETURN 95 C199J1 2 CONFIG MODULE DATA RX 96 C199J1 3 SPARE DIO DISC IN 97 GND OPEN RESERVED WARNING RESET 98 GND OPEN RESERVED ON SIDE AWP 99 MASTER GND OPEN SPARE DIO DISC IN 100 28V 0PEN CROSS 28V YD CLUTCH IN 101 AT DISCONNECT GND OPEN 102 FIGURE 8 11 FGC RESET GND OPEN 103 FMS RS 232 COMMON 104 FMS RS 232 DATA RX 105 FIGURE 8 3 FMS RS 232 DATA TX C190J1B 106 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document 10 0 0 0 0 Function Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 AIL SERVO DRIVE H C190J1C 1 CCW DRUM ROTATION L 2 ELEV SERVO DRIVE 3 CCW DRUM ROTATION L 5 CROSS YD PWR SENSE OUT 28 V OPEN TRIM UP 28V GND SPARE H A 429 XMTR 5 L TRIM DN 28V GND 28V YD BRAKE OUT I
227. tion on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 1 cont IC 800 IO BP Function Connector Pin Connects To 0 WX 1 RANGE DN OUT 190J1B 30 24 GND OPEN C190J1B 30 E190J1B 30 0 SPARE DIO DISC OUT 31 28V 0PEN 0 SPARE DIO DISC OUT 28V 0PEN RSB RESERVED AP OFF HORN GND OPEN FIGURE 8 15 RSB RESERVED DP1 RESET GND OPEN SPARE DIO DISC OUT GND OPEN SPARE DIO DISC IN GND OPEN SPARE DIO DISC OUT GND OPEN RSB RESERVED CAUTION RESET GND OPEN FIGURE 8 11 CDU VALID GND OPEN 120J1 i SEC RADIO TUNE GND OPEN ALT ALERT HORN GND OPEN FIGURE 8 15 WX ON GND OPEN 5901 0 61J1 R 61 1 C190J1B 45 E190J1B 45 WARNING ANNUN GND OPEN DU 2 REV GND OPEN RAD ALT TEST GND OPEN 4 FIGURE 8 13 EICAS RIGHT SEL GND OPEN E135J1 11 DAUI REV FIGURE 8 2 GND OPEN SG TEST IN 135J1 49 GND OPEN 115J2 15 C115J2 15 SPARE DIO DISC IN GND OPEN RSB RESERVED BC RESERVED BC RESERVED BC RESERVED 6 BC IDENT 2 190J1B 57 GND OPEN 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC N
228. tle page of this document SYSTEM Honeywell FALCON 900EX e Set RADAR knob between RCT and WX again and make sure that VAR is not displayed lf it is repeat this step f Adjust the GAIN control on the WC 880 Weather Radar Controller until the ground clutter display is symmetrical g Do not touch the manual GAIN control once the display is adjusted properly h Select RCT on off on off within three seconds by setting RADAR knob between RCT and WX This causes the WU 880 to exit the roll compensation mode When VAR is displayed again the roll compensation mode has been exited i Set variable or preset GAIN as desired j This compensation data is now stored in nonvolatile memory in the WU 870 and will not be erased when power is removed from the system C Repair Procedures Not Applicable 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX SECTION 5 SHIPPING HANDLING AND STORAGE Refer to manual Pub No 09 1100 01 for detailed procedures for preparing all System components for storage or shipment 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX Blank Page 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to t
229. to the restrictions on the title page of this document Honeywell SYSTEM MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 Function Connector Pin SPARE FWC DISC IN C190J01A 44 GND OPEN FMS DATA LOADER H 45 DATA OUT FMS RS 422 TX L 46 FMS DATA LOADER RS 232 TX FMS DATA LOADER RS 232 RX BC DL RS 232 COMMON DISPLAY CONTROL 1 L IOP RS 422 RX CH SPARE CARD RESERVED SPARE CARD RESERVED V L 2 A 429 RCVR 21 L IOP RS 422 RX IAC IDENT 1 GND OPEN SPARE en H L SPARE in L E IOP RS 422 TX L IDENT 0 GND OPEN WX CONTROL DATA 2 H IOP RS 422 RX L FMS DATA LOADER f H 63 DATA IN FMS RS 422 RX 1 C190J1A 64 Connects To 190J1A 45 E190J1A 45 123J1 G 190J1A 46 E190J1A 46 FIGURE 8 3 115J1 8 E190J1A 49 115J1 7 E190J1A 50 FIGURE 8 2 SIGNAL GND 59J1 e 190J1A 61 E190J1A 61 59J1 f 190J1A 62 E190J1A 62 123J1 T 190J1A 63 E190J1A 63 123J1 S 190J1A 64 E190J1A 64 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont INTEGRATED AVIONICS COMPUTER IAC NO 2 cont IC 800 0 BP Function Connector Pin Connects To FMS DATA LOADER H C190J1A 65 CTS IN FMS
230. tor Tighten locking nut and install safety wire d Assemble locking nut and washer to rod end of actuator INSTALLATION CRITICAL THREAD ENGAGEMENT WITH ROD END BEARING MUST BE 0 56 IN 14 22 MM MINIMUM e Thread Rod end bearing to actuator Tighten locking nut and install safety wire f Attach fork end of actuator to airframe fitting and secure with bolt washer castellated nut and cotter pin g Attach rod end bearing of actuator to airframe fitting with bolt and bushing h Check alignment in accordance with the aircraft maintenance manual i Secure actuator rod end attachment bolt with washer nut and cotter pin j Connect aircraft cable connector to actuator connector 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM Honeywell FALCON 900EX B Adjustment Procedures Not Applicable C Repair Procedures Not Applicable 25 Procedure for the SM 810 Autothrottle Servo A Removal and Reinstallation Procedure 1 Remove SM 810 Autothrottle Servo a Release bridle cable tension b Cut safety wire on four nuts securing retaining plate and remove and set aside screws lock washers and retaining plate c Remove and set aside four cable keepers d Cut safety wire and remove and set aside two screws securing swaged cable terminals to drum e Unwrap bridle cables from drum f Remove and
231. two test connectors located in the cockpit in the pilot s side panel below the DL 900 Data Loader Connect the PC to the adapter harness Connect the PC to external power and power up the aircraft and the PC Using the PC checklist software select the upload or download checklist menu as applicable and follow the instructions When the checklist upload download is complete power down the PC and the aircraft C Repair Procedures Replacement of the Battery CAUTION THE BATTERY IS LITHIUM AND MUST BE DISPOSED OF PROPERLY 1 Check battery a Locate the battery housing this is positioned at the left rear corner adjacent to the fan Loosen the three screws that hold the battery cover and remove the cover NOTE If a Honeywell quality inspection seal is covering one of the screws remove the seal completely using isopropyl alcohol Locate the small connector connected to the battery Probe the contacts of the connector and measure the battery voltage while under load NOTE The three pins on the connector have positive voltage on the center pin and the other two pins are both common and are attached to the negative terminal of the battery Replace any batteries with a voltage reading of less than 2 4 volts DC 2 Remove battery a Locate the 50 pin test connector on the IAC it is positioned under a small plate on the front panel Remove the two screws that hold the plate to gain access to the test
232. ubject to the restrictions on the title page of this document SYSTEM Honeywell MAINTENANCE MANUAL FALCON 900EX Table 3 1 Interconnect Information cont Table 4 1 cont Connector Wire Gauge Limitations Unit Component Connector Wire Gauge 136 137 DA 800 TR2P106P106P 0001 210 212 22 AWG 149 GNSSU M83723 77R2041N 41 22 AWG 170 LASEREF III BKAD2 313 30001 172 MSU MS3126F18 32S 32 20 AWG 190 IC 800 TRAP 424 Q 22 AWG 106P106P106P106P 0001 Aircraft Test Connectors The M1558 1563 avionics system requires the installation of two test connectors to fully utilize the systems built in test diagnostic capabilities These connectors are defined in Figure 8 3 The plan is to install the same connectors and pinout on all similarly equipped aircraft to enable the use of a common test equipment harness The test connectors must be installed in the cabin area to enable convenient ground and flight data collection 22 05 21 Sop 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont 4 2 Interconnect Requirements 4 2 1 Polarities Installing the system in accordance with the interconnect information defined in this document will result in the following servo polarities Aileron Servo Clockwise Roll left Elevator Servo Clockwise Pitch down R
233. udder Actuator Extend Yaw right If it is impossible to maintain the above relationships the aileron and elevator servo drive drum rotation direction can be changed by interchanging the connections to pin A with pin B and pin L with pin N on the appropriate servo The rudder linear actuator can be reversed by interchanging the connections to pin A with pin B and pin M with pin N Engage Interlock The Integrated Avionics Computer is electrically keyed to prevent the wrong computer from operating in an aircraft Servo Drive Electrical Keying The engage clutch of the servo drive is electrically keyed as a function of power gear ratio to prevent the wrong servo from engaging Maintenance Test Maintenance Test is initiated by pressing the maintenance bezel button located on the appropriate menu of the EID display bezel The maintenance test function is interlocked with weight on wheels WOW and airspeed to ensure activation is not possible during flight 22 05 21 Sep 1 1996 Use or disclosure of information on this page is subject to the restrictions on the title page of this document SYSTEM MAINTENANCE Honeywell MANTEN FALCON 900EX Table 3 1 Interconnect Information cont Circuit Breaker Selections This paragraph provides information needed for selecting circuit breakers for the avionics system defined by Modifications 1558 and 1563 Table 4 2 quantifies the maximum power and current requirements for each system compon
234. y Controller 4 8 9 Procedure for the DL 900 Data Loader 4 11 10 Procedure for the DU 870 Display Units 4 12 11 Procedure for the GC 810 Flight Guidance Controller 4 14 12 Procedure for the Global Navigation System Sensor Unit GNSSU 4 17 13 Procedure for the IC 800 Integrated Avionics Computer IAC 4 18 14 Procedure for the IM 803 Installation Module 4 24 15 Procedure for the Inertial Reference Unit IRU 4 25 16 Procedure for the IRU Mounting Tray Fan Filter 4 26 17 Procedure for the IRU Mounting Tray Fan 4 27 18 Procedure for the IRU Mounting 4 29 19 Procedure for the Mode Select Unit MSU 4 34 20 Procedure for the RC 820 Reversionary Controller 4 35 21 Procedure for the RC 841 Reversionary Controller 4 37 22 Procedure for the RT 300 Radio Altimeter Receiver Transmitter 4 39 23 Procedure for the SM 200 Servo Drive and the SB 201 Drum and Bracket Assembly 2 2 Sar nae ee E MEE Ru as Ba 4 41 24 Procedure for the SM 725 Linear Actuator 4 43 25 Procedure for the SM 810 Autothrottle Servo 4 45 26 Procedure for the WC 880 Weather Radar Controlle

SMM:PRIMUS 2000 Integrated Avionics System:Falcon 900EX

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