INSTALLATION MANUAL - Ameri
Contents
1. 22 Normal operating condition 14 Vdc 28 Vdc System System Maximum 15 1 30 3 Nominal 13 8 27 5 Minimum 12 4 24 8 Emergency 10 0 20 0 Category B Equipment designed to withstand the transient voltage characteristics specified by RTCA DO 160B 2 3 1 4 ACCESSORIES SUPPLIED 1 4 1 Installation Kit Part No IK 3502001 IK 3502002 IK 3502003 IK 3502004 IK 3502005 IK 3502006 Description Connector Socket 15 Pin with Wiring Harness Assembly Pneumatic Hose Pneumatic Fitting T type Pneumatic Fitting Straight type Placarding Mounting Tray INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 SECTION Il INSTALLATION AND TEST UNPACKING AND INSPECTING EQUIPMENT The Altitude Reporter should be unpacked with extremely care Visual inspection of the equipment for evidence of damage incurred during shipment Any claim should be promtly filed with the transportation company Save the shipping container to subtantiate the claim MECHANICAL INSTALLATION The AK 350 Altitude Reporter is normally mounted in the equipment rack or cabin area or beneath the instrument panel which is the temperature controlled environment either pressurized or non pressurized area It should be located away from heater vents and fresh air vents temperature Its mounting base should be adequately secured in accordance with all applicable FARs The mounting location should allow a short pressure line from the2. Automatic Pressure Altitude Reporting Code Generating Equipment Model AK 350 Technical Standard Order C88a Your applications dated August 22 1988 and December 29 1989 requesting the issuance of a Technical Standard Order TSO authorization in accordance with the procedural requirements of Federal Aviation Regulation FAR Part 21 Subpart 0 has been reviewed Based upon your data and statement of conformance certifying your article has met the requirements of FAR Part 21 Subpart 0 and the minimum performance standards of TSO C88a Ref FAR 21 305 b authorization is hereby granted The following technical data are considered to fulfill the requirements for a TSO authorization and are being retained in our files l Drawing Nos 350201 AK 350121 Rev A 2 Document Nos IM 3501001 dated 8 17 89 QTP 3501005 dated 8 17 89 ATP 3501002 dated 8 18 89 TSPQ 3501000 dated 8 18 89 The quality control procedures contained in your quality control manual Ameri King Corp Quality Assurance Manual Revision A dated November 9 1989 is currently on file at the Los Angeles Manufacturing Inspection District Office and your statement that those procedures will be applied to the manufacture of the subject article at the above address are considered adequate in accordance with FAR 21 143 Effective this date you are authorized to use TSO procedures for the subject Automatic Pressure Altitude Reporting Code Generating Equipment
3. Black 14 Vdc Red or 28 Vdc A1 A2 A4 B1 B2 B4 cl C2 c4 Strobe DC Ground Power Input n Im m OF A4gl kK Power Gnd AK 350 a ERS ATC TRANSPONDER ALTITUDE REPORTER WILCOX 1014A Figure 2 20 Interconnect Schematic Diagram All wires are 22 AWG 17 24 2 5 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 LIST OF MAJOR COMPONENTS In addition to the Altitude Reporter AK 350 followings are list of the major components List of some compatible transponders which make up the equipment system LIST OF SOME COMPATIBLE TRANSPONDERS MANUFACTURERS CURRENT MODELS OLDER MODELS BENDIX TR 542 TPR 2060 TPR 660 TR 641A B CESSNA RT 359A RT 459A RT 859A COLLINS TDR 950 950L EDO AIR RT 777 GENAVE BETA 5000 KING KT 76A KT 76 KT 78 KT 79 KT 78A KXP 750A KT 75 NARCO AT 150 AT 5 AT 6 AT 6A AT 50 AT 50A RADAIR 250 TERRA TRT 250 WILCOX 1014A CALIBRATION The AK 350 Altitude Reporter is calibrated at the factory to a pressure data traceable to the National Bureau of Standards When the AK 350 is installed in the aircraft it must be calibrated to the primary flight altimeter per Advisory Circular 43 6A so as to comply with FAR 91 36 b and FAR 91 177 18 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 PILOT STATIC TEST SET PRIMARY ALTIMETER ALTITUDE REPORTER AK 350 TRANSPONDER TEST SET Transponder Test Set IFR
4. ATC600A or MICHAEL 730 or Altitude Read out or equivalent Figure 2 21 Test Set Up 19 2 5 1 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Calibration Procedure See Figure 2 21 for Test Set Up Step 1 Connect a static pressure system tester to the airplane The AK 350 Altitude Reporter must be connected to the aircraft static line near the flight altimeter and the two altitude adjustment screws must be accessible Apply power to the AK 350 Altitude Reporter and the ATC Transponder Test Set Set primary flight altimeter to 29 92 in hg Allow a minimum of 15 minutes warm up time Apply static pressure system tester to obtain a flight altimeter reading of 29 900 ft Slowly decrease pressure and read the flight altimeter at transition point 29 900 30 000 feet Transition point is indicated on the Transponder Test Set If necessary adjust the HI pot of the AK 350 until the transition point at decreasing pressure is 29 950 20 feet as read on the primary flight altimeter Note 1 The Transponder Test Set reading should match with flight altimeter reading not with the static pressure system tester Note 2 Because mechanical primary flight altimeter pointers are not totally frictionless therefore tap lightly on the primary flight altimeter with a screwdriver handle to eliminate friction before taking any reading Note 3 A leaky static system will make calibration difficult if n
5. You may identify this article with the applicable TSO markings as required by TSO C88a 28 INSTALLATION MANUAL INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 3350 ALTITUDE REPORTER ENCODER MODEL AK 350 Luftfahrt Bundesamt 2 Luftfahrt Bundesamt Postfach 3054 D 3300 Braunschweig As recipient of this TSO authorization except as provided in FAR 21 3 d inschreiben you are required to report any failure malfunction or defect in any product or part manufactured by you or your contracted suppliers and which Ameri King Corp you have determined has resulted or could result in any of the occurrences 20902 Brookhurst St listed in FAR 21 3 c The report should be communicated initially by Unit 107 telephone to the Manager Technical and Administrative Branch ANM 103L Huntington Beach 213 988 5300 within 24 hours after it has been determined the failure has CA 92646 occurred and followed up with a written notice FAA Form 3330 2 Malfunction or Defect Report or other appropriate format is acceptable in USA transmitting the required details As requtred by FAR 21 613 b you must also notify the FAA when you no longer manufacture a TSO approved article Bitte bei Antwort angeben Ihre Zeichen und Nachricht vom zen 221 6 8 92 ges ay Aug ria This authorization pertains only to manufacturing operations at the above address This office must be notified in advance of any proposed facility relocation to preclude interrupti
6. _ Kapalle a y INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Bundesamt f r Zvilufttahrt BAZL Accomeccanica SA Office f d ral de l aviation civile OFAC Aeroporto Cantonale di Loc rno Ufficio tederale dell aviazione civile UFAC 6596 Gordola Federal Office for Civil Aviation FOCA Authorisation for Installation and Operation of Ameri King AK 350 Blind Altitude Encoder Based on the documents listed in attachment 1 the Swiss Federal Office for Civil Aviation authorizes the installation and operation of the AK 350 Altitude Reporter in Swiss registered aircraft in the authorisation class 2 Base of conformance TSO C88a RTCA DO160B Limitations The limitations stated by the environmental categories must be considered The system approval includes the following components AK 350 Altitude Reporter CLBA SLM KXXXXXZBBXKXX The Swiss type acceptance is based on chapter 3 of Verordnung ber die Zulassung und den Unterhalt von Luftfahrzeugen dated July 8 1985 The documentation provided to the Federal Office for Civil Aviation in support of the acceptance process is listed below and will be kept in our files Aromeccanica application with Ameri King Specification AK 350 Encoder 2 March 1993 Performance and accuracy of production components must correspond to the type approved The applicant manufacturer will inform the Federal Office for Civil Aviation about all further design chan
7. data on the Altitude Encoder AK 350 as and when these are published Yours faithfully ho he Kell Werner K Kapalle Chief Certification Equipment Section 31 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 BUNDESREPUBLIK DEUTSCHLAND LUFTFAHRT BUNDESAMT MUSTERZULASSUNGSSCHEIN Type Certificate Nr 10 221 6 Das nachstehend bezeichnete Luftfahrtger t ist als Muster zugelassen auf Antrag von Ameri King Corporation Huntington Beach CA 92646 USA Dieser Musterzulassungsschein ist auf Grund der die Musterzulassung betreffenden Bestimmungen des Luftverkehrsgesetzes und der Luftverkehrs Zulassungs Ordnung In der am Tage der Ausstellung geltenden Fassung erteilt Die Musterzulassung gilt gem zugeh rigem Ger te Kennblatt Nr 10 221 6 Bezeichnung des Ger temusters AK 350 Ger teart Kodierender H henmesser ohne Anzeige Die Musterzulassung kann in den in 4 Abs 2 der Luftverkehrs Zulassungs Ordnung vorgesehenen F llen widerrufen werden On application of and in accordance with the German Certification Regulations as In force to day for the following product the Type Certificate Is issued The Type Certificate Data Sheet No is part of the Type Certificate The type certification may be revoked by the LBA in cases Provided in the German Certification Regulations Unterschrift Signature Datum der Ausstellung Date of issue Non 1 ae LL A Braunschweig 10 August 1992 sch 35
8. data to the ground station set forth in the International Standard Code for SSR Pressure Altitude Transmission The AK 350 model has an altitude range from 1 000 feet to 30 000 feet The Altitude Reporter AK 350 is a remote mounted equipment that is fully automatic in operation The companion ATC Transponder normally controls the operation of the Altitude Reporter by automatically enabling or disabling its operation This is done by pulling up to logic LOW to enable or pulling down to logic HIGH to disable the STROBE Pin 6 line of the Altitude Reporter It is in operation enabled any time the Transponder is set to the Altitude mode Mode C of operation The digital altitude data is imhibited disabled any time the Altitude mode is turned off or to the Ident mode Mode A 24 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Power to the Altitude Reporter is automatically turned on whenever the companion Transpoder is switched to STANBY mode or ON mode or ALTITUDE mode IMPORTANT OPERATION NOTE During in flight operation if the altitude information is reguested to turned off by the ATC Controller the companion Transponder should be switched to the STANBY mode not to the OFF mode When the power is re activated a warm up time is reguired in order for the Altitude Reporter to function properly If the companion Tranponder does not have switched power output pin to the Altitude Reporter an
9. extremely reliable equipment equipment rack mounted designed to meet TSO C88a requirements The AK 350 Altitude Reporter is connected to the aircraft pneumatic static system and output to the ATC Transponder It converts altitude pressure into altitude digital data output to ATC Transponder When the ground station requests for reporting the altitude the Transponder will transmit the altitude digital data to ground station set forth in the International Standard Code for SSR Pressure Altitude Transmission The AK 350 model has an altitude range from 1 000 feet to 30 000 feet 2 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 1 3 TECHNICAL CHARACTERISTICS SPECIFICATIONS CHARACTERISTICS TSO COMPLIANCE TSO C88a PHYSICAL CHARACTERISTICS e Width l 3 50 inches e Height 2 00 inches e Length 4 75 inches Weight 0 40 Ibs Mounting Equipment Rack Mounting type ALTITUDE RANGE From 1 000ft To 30 000ft Basic Part No or 35 40 42 50 60 62 80 K ft various Part No GENERAL SPECIFICATIONS Operating Temperature Storage Temperature 20 deg C to 55 deg C 55 deg C to 85 deg C Power Input 10 32 Vdc After Warm Up 13 8 Vdc 0 20 Amp typical 27 5 Vdc 0 17 Amp typical 13 8 Vdc 0 60 A for 1 min 27 5 Vdc 0 59 A for 1 min During Warm Up BLIND ENCODER OUTPUT Per the International Civil Aviation Organization altitude transponder code Referenced to 29 921 in h
10. s 337 or 8130 THE IMPLIED WARRANTY AND ALL OTHER IMPLIED WARRANTIES ARE HEREBY EXCLUDED AMERI KING CORP MAKES NO OTHER WARRANTY OR REPRESENTATION OF ANY KIND WHATSOEVER EXPRESSED OR IMPLIED AND ALL IMPLIED WARRANTIES INCLUDING ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE ARE HEREBY DISCLAIMED AMERI KING CORP S MAXIMUM LIABILITY HEREUNDER IS LIMITED TO THE PURCHASED PRICE OF THE PRODUCT IN NO EVENT SHALL AMERI KING CORP BE LIABLE FOR ANY CONSEQUENTIAL INDIRECT INCIDENTAL OR SPECIAL DAMAGES OF ANY NATURE ARISING FROM THE SALE OR USE OF THE PRODUCT WHETHER BASED IN CONTRACT TORT STRICT LIABILITY OR OTHERWISE REPAIR SERVICE All equipments manufactured by Ameri King Corp must be repaired at the facility of Ameri King Corp All the repair services shall be performed and completed within 3 days upon repairing estimate is approved by equipment user or installation dealers 27 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 APPENDIX A TSO Approved Letters from FAA USA GERMANY and SWITZERLAND a US Department NORTHWEST MOUNTAIN REGION of Transportation TRANSPORT AIRPLANE DIRECTORATE Federal Aviation AIRCRAFT CERTIFICATION SERVICE Administration LOS ANGELES AIRCRAFT CERTIFICATION OFFICE 3229 EAST SPRING STREET LONG BEACH CA 90806 2425 FEB 20 1990 Ameri King Corp 20902 Brookhurst Street Unit 107 Huntington Beach California 92646 Gentlemen Ameri King Corp
11. Appendix E FAR 43 and Advisory Circular 43 6A Set the primary flight altimeter barometric to 29 92 in Hg Select several of the following Corr spondence test points chosen by the Calibrating Technician from 1 000 feet to the maximum operating altitude of the aircraft or 30 000 feet for both increasing pressure and decreasing pressure 21 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Correspondence Transition for Transition for Test Point Decreasing Pressure Increasing Pressure 1 000 ft 1 050 125 ft 950 125 ft O ft 50 125 ft 50 125 ft 2 000 ft 1 950 125 ft 2 050 125 ft 6 000 ft 5 950 125 ft 6 050 125 ft 10 000 ft 9 950 125 ft 10 050 125 ft 14 000 ft 13 950 125 ft 14 050 125 ft 20 000 ft 19 950 125 ft 20 050 125 ft 25 000 ft 24 950 125 ft 25 050 125 ft 30 000 ft 29 950 125 ft 30 050 125 ft Maximum Correspondence Error shall be 125 feet as read on the primary flight altimeter NOTE 1 NOTE 2 If the aircraft ceiling altitude is less than 30 000 feet perform the same above procedure for its ceiling altitude i e from 1 000 feet to maximum aircraft ceiling altitude Because mechanical primary flight altimeter pointers are not totally frictionless therefore tap lightly on the primary flight altimeter with a screwdriver handle to eliminate friction before taking any reading A leaky sta
12. DC Powe DC Ground 15 Black pe em poendi beans oceni ocan De Gna DC Gna ji No Connection 114 Red Wht No Connect No Connect No Connect Note 2 No Connection Leave Pin Open for P N AK 350 AK 35035 AK 35040 AK 35050 t AA This Connection is required for P N AK 35080 only Bee al m ee cores Note 1 No Connection Leave Pin Open for P N AK 350 General Note It is important that Refer to GPS Manufacturer Installation Manual for Actual Installation ER a ION FR a ICON WARE RN FIGURE 2 8 ALTITUDE ENCODER INTERCONNECT SCHEMATIC DIAGRAM WITH NON STROBE GPS 17 BEER E A O Er a DAA RA BERER u iE NE N RE OSE AV N d 10 uedg uid eABe7 UONDeELLOJoON L SION A A A en UO OBOSE MW N d 10 Pesnbal 81 uonseuuog sul __ O90SEAV OSOSE AV OPOSE NV SEOSE NV OSE NV N d JO uedo uid onee UONIBUUO ON 7 eN AH AAA 0 aaa ur em Ba 1 ar WOO ON UWP9y yi Be a eee ae NN NO oc a yela SL punga JA pf fer reef ueno PET sa Ao rs sar pp OOO rn an za pT rns an sion nei pad pre ee ee nae eo le ee ee ee Oe ea Eee ae ee ee ee eek MeN ho ae ee a i E OO pal Fp ee MONA E Be BAA Seel dee IAE a se a je ee OM ee Br a ee i EOE ee ee eh re ee ee OM En ee ee ee A SAA AAPP TST TOR Se II 101000010177 CC DNII INEWV SEGOONG Lin er ee ee ee OMA i ALT ENCODER AMERI KING SIGNAL AK 350 FUNCTION Pin No Wire Co
13. Document No IM 3501001 Rev NC dated 8 17 89 INSTALLATION MANUAL ALTITUDE REPORTER ALTITUDE ENCODER MODEL AK 350 AMERI KING CORPORATION 17881 Sampson Lane Huntington Beach CA 92648 Tel 714 842 8555 Fax 714 842 4235 Web Site www ameri king com Email sales ameri king com INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 IMPORTANT NOTES The followings are General Specifications for different part No Model AK 350 Part No AK 350 Altitude Range 1 000ft to 30 000ft Temp Range 20 deg C to 55 deg C Model AK 350 Part No AK 35035 Altitude Range 1 000ft to 35 000ft Temp Range 40 deg C to 55 deg C Model AK 350 Part No AK 35040 Altitude Range 1 000ft to 40 000ft Temp Range 40 deg C to 55 deg C Model AK 350 Part No AK 35050 Altitude Range 1 000ft to 50 000ft Temp Range 50 deg C to 55 deg C Model AK 350 Part No AK 35060 Altitude Range 1 000ft to 62 000ft Temp Range 50 deg C to 55 deg C Model AK 350 Part No AK 35080 Altitude Range 1 000ft to 80 000ft Temp Range 50 deg C to 55 deg C cr rrr ees aru SSS The following pages are applicable to all Part No for 35 000 ft 40 000ft 50 000ft 60 000ft and 80 000 ft configurations Page 8A Connector Pin Function Interface with Strobe and None Strobe type ATC Transponder Page 22A Data Correspondence Test Point Table AA ad PW
14. ION 2 ji i Ta ON POULOZ ON FEUD ON Peuuog ON 900005 ON POULO ON POULO ON a UNWPSYy it TUopseuuogon pup a pusjer pup sz uokzez pus a unas punar zi 7 ____egis Ppunusga wewod og Mirzz IMd g warigurz Mde Y manzi end IQ i E pey g 1 uy N pus a user pup sz Wuokzzz pus a tunas punoo zi Ould 9 POULOJ ON FOSULOS ON eUUOD ON eUUICD ON EUUCD ON POULO ON PULOJ ON Zeion GUAM za Peuuo ON 30euuoo ON L6JON OZ LEON Lz weuuoson T BION 8 PewUCD ON Fi sion users mil y z z H 0 T Tena onana 4 vO a ag umoug zo vb umwgme ii W bL L __ 6uei9 017 ya OL mower 6 za 6 ueaid s ae El enig y vv 9 con A 7 4 pasa zza als a OL Mig S 0 10M 21x ojwloima 4 T 40109 OLIM ON id NOLLONNS kio avi JA 0S NV T 1 FTWNO9IS jamaa unse ONDEIVANV Y3009N3 LIV 057 sepuodsusu sepuodsum INSTALLATION MANUAL ALTITUDE REPOATER ENCODER MODEL AK 350 Alt Mode Enable Not Connected Al A2 A4 B1 B2 B4 A1 White A2 Gray A4 Blue B1 Green B2 Yellow B4 Orange Al A2 A4 B1 B2 B4 C1 C1 Tan c1 C2 C2 Brown C2 c4 C4 Violet c4 Strobe Strobe
15. N AE a v Figure 2 1 Installation Drawing 7 0 156 so INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Not Connected Al A2 A4 B1 B2 B4 Cl C2 c4 Strobe DC Ground 14 28 Vdc AT A2 A4 B1 B2 B4 C1 C2 c4 Strobe DC Ground Power Input A1 White A2 Gray A4 Blue B1 Green B2 Yellow B4 Orange C1 Tan C2 Brown C4 Violet Strobe Pink DC Ground Black 14 Vde Red or 28 Vdc Sw Power AK 350 With Strobe Type ALTITUDE REPORTER ATC TRANSPONDER Figure 2 2 Connector Pin Function interface with Strobe type ATC Transponder Not Connected Al A2 A4 B1 B2 B4 ci C2 c4 Strobe DC Ground Power Input A1 White A2 Gray A4 Blue B1 Green B2 Yellow B4 Orange C1 Tan C2 Brown C4 Violet Strobe Pink DC Ground Black 14 Vdc Red Al A2 A4 B1 B2 B4 C1 C2 C4 Strobe DC Ground 14 28 Vdc or 28 Vdc Sw Power AK 350 Without Strobe Type ALTITUDE REPORTER ATC TRANSPONDER Figure 2 3 Connector Pin Function interface with Non Strobe type ATC Transponder 8 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 14 Not Connected 7 D2 D2 D4 D4 WA et A1 White ree ie A2 Gray re Aa 4 A4 Blue AA Bils B1 Green B1 sho B2 Yellow 82 84 lio B4 Oran
16. ON OFF Switch and a Power Off Light may be incorporated See Figure 2 5 above 25 4 1 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 SECTION IV WARRANTY LIMITED WARRANTY All equipments manufactured by Ameri King Corp are guaranteed against defective materials and workmanship for a period of one and a half years after purchase Any equipment found to be defective due to material and workmanship during this limited warranty will be repaired and put in original manufactured operating condition An option of extended three years limited warranty will become valid at the end of the first one and a half years which will warrant to the original owner This Ameri King Corp warranty is void unless the Warranty Registration Card is filled out and returned to Ameri King Corp within 10 days after original purchase Ameri King Corp s liability under this warranty is limited to servicing repairing replacing or adjusting any equipment returned prepaid to the factory by express written or oral authorization for that purpose and to repair or replace defective parts thereof Repaired equipment will be returned to the equipment user freight pre paid Shipping charge will be paid one way only by Ameri King Corp Upon discovery of a condition believed to be caused by a defect in manufacturing Ameri King Corp must be notified No equipment to be shipped to Ameri King Corp without prior authorization Any equipment r
17. Pink Strobe DC Ground DC Ground Black Sig Com Power Input 14 Vdc Red Dig Power AK 350 ATC TRANSPONDER ALTITUDE REPORTER NARCO AT 5 AT 6A Figure 2 17 Interconnect Schematic Diagram All wires are 22 AWG Not Connected Al A2 A4 B1 B2 B4 c c2 c4 Strobe DC Ground Power Input A1 White A2 Gray A4 Blue B1 Green B2 Vellow B4 Orange C1 Tan C2 Brown C4 Violet Strobe Pink DC Ground Black 14 Vde Red Al A2 A4 B1 B2 B4 c1 C2 c4 Strobe Dig Power AK 350 ATC TRANSPONDER ALTITUDE REPORTER NARCO AT 50A AT 150 Figure 2 18 Interconnect Schematic Diagram All wires are 22 AWG 16 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL Ak 350 Not Connected AT A2 A4 B1 B2 B4 C1 C2 c4 A1 White A2 Gray A4 Blue B1 Green B2 Yellow B4 Orange C1 Tan C2 Brown C4 Violet Strobe Pink DC Ground Black 14 Vde Red Al A2 A4 B1 B2 B4 ci c2 c4 Strobe DC Ground Power Input Sig Com Dig Power AK 350 ATC TRANSPONDER ALTITUDE REPORTER RADAIR 250 Figure 2 19 Interconnect Schematic Diagram All wires are 22 AWG Not Connected Al A2 A4 B1 B2 B4 ci C2 c4 A1 White A2 Gray A4 Blue B1 Green B2 Yellow B4 Orange C1 Tan C2 Brown C4 Violet Strobe Pink DC Ground
18. R gt 2 1 2 2 2 3 2 4 2 5 2 6 2 7 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 TABLE OF CONTENTS Table of Contents 2essseseesessennnneenennnennnan nennen 1 SECTION GENERAL INFORMATION SCOPE A E T E E EE EEEE 2 Description ae rare 2 Technical Characteristics AN hed pe 3 Accessories Supplied w 5 SECTION Il INSTALLATION CALIBRATION AND TEST Unpacking and Inspecting Equipment 6 Mechanical Installation 6 Electrical Installation 6 List of Major Components serrera 18 Calibration a antenne ER 18 Data Correspondence Test 21 Placarding nn se ee AA MABAWA IAA 23 SECTION ili OPERATION SECTION IV WARRANTY AND SERVICE Limited Warranty wwwwnawanenna nennen 26 Repair Service IA iia 27 A 1 1 1 2 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 SECTION GENERAL INFORMATION SCOPE This manual contains information necessary for the installation calibration test and operation of the Altitude Reporter model AK 350 manufactured by Ameri King Corporation California U S A DESCRIPTION The AK 350 Altitude Reporter is an integrated circuit technology based equipment It is a highest standards of quality and
19. dc Red or 28 Vdc Power Input Power AK 350 ALTITUDE REPORTER ATC TRANSPONDER Power off Light 14 28 Vdc bus On Off Panel Switch Figure 2 5 Power pins interface with Non Switched power output type Transponder All wires are 22 AWG 9 __ traneponder_ Transponder Transponder Transponder Transponder Transponder Transponder ALT ENCODER AMERI KING GARMIN ups tech BECKER BENDIX COLLINS TERRA _SIGNAL _ AK350 GTX 220 327 SL70_ ATC 2000 frer zosorsector ssorssoll TRT 250 KT 78 FUNCTION Pin No Wire Color P102 __ PinNo PinNo PinNo PinNo Pin No PinNo eo ee lo ee ee Al 1 EA O 3 ea me a ie 6 AI pee A Pie Grey AA AN ERA a A aa IIA BI 6 Greeny 8 as Ss 5 Tb 1 I B2 _ 9 Yelow 11 14 198 90 1 5 73 tT B4_ HOC Orange 12 32 986 ta ta mt Ct iia wai 10 16 2 a 7 ae a 62 f3 Brown aaa 5 HT at T ___C4 12Molet Purple Biue He A Se ze D4 Tr tGreen Note 1 18 Note 1 38 Note 1 23 Note 1 No Connect No Connect No Connect No Connect D2 7 BikWht Note 2 No Connect No Connect No Connect No Connect No Connect No Connect No Connect 1 Strobe DC Ground 6 Pink 13 0 Gnd 2 DC Gnd 24 DC Gnd DC Ground DC Ground 12 DC Gnd 5 DC Gna DC Power In 8 Red _____ 15 Dc Power 1 DC Power 6 DC Power DC Powe
20. digitizer to the same static line as the flight altimeter See fugure 2 1 for Installation drawing During installation the installation must provide provisions for access to the two adjustment screws for Calibration purpose ELECTRICAL INSTALLATION The AK 350 Altitude Reporter is designed to operate on a 14 Vdc or 28 Vdc aircraft bus See Figures 2 2 2 3 for Connector Pin Function interface with Strobe type Transponder and Non Strobe type Transponder repectively See Figures 2 4 2 5 for Power pins interface with Switched power output type Transponder and Non Switched power output type Transponder respecttively See Figures 2 6 thru 2 20 for Interconnect Schematic Diagrams It is recommended that all wires are 22 AWG 6 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 15 32 32 UNS 2A 1 8 27 NPT X 50 DEEP 2 00 Pw aa lt 3 50 gt ei 4 50 4 70 Unit Connector D Subminiature Receptacle 15 Pins Mating Acessories supplied Prefabricated Molded Cable Assy with 2 Places D Subminiature Plug 15 a Color Coded 22 AWG Wires or D Subminiature Plug 15 Female Crimped 4 70 Pins with Backshell ty 1 8 Dia Hole 4 00 4 50 HDP 20 Series A ed AMP Inc or Equivalent z YA u reer 2 ag e A A D EMBOSS 3 PL 3 000 OUTLINE DIMENSIONAL DWG MOUNTING TRAY x PEMNUT CLA 440 1 0 688 0 18 0 688 0 688 a o
21. eturned to Ameri King Corp should be accompanied by a failure report in writing giving full particulars in support of the claim This limited warranty does not cover or apply to any of the followings including misuse of the equipment installation or operation not in accordance with factory instructions accidents or negligent damage alterations of any manner repair by other factory changes in calibration occuring as a result of normal use of the equipment the cost of labor material or other expense incidental to the repair installation 26 4 2 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 removal from the aircraft or replacement of the equipment damaged during shipment or installation any personal injuries or damage to property resulting from the installation or the operation of the equipment or the failure of the equipment or any part thereof the equipment user assumes the risks of all such injuries or damage In such cases the repair will be billed at cost An estimate will be submitted for approval before repair is initiated Any equipment which is returned for warranty and found not to be defective shall be charged a minimum handling and service charge and returned C O D No warranty will be activated for Ameri King Corp products unless the installation is approved by an FAA Certified Installer and the warranty card is completed by the supplying dealer or upon receipt by Ameri King Corp of form
22. g at all times Mode C Compatible with all transponders in use today INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 SPECIFICATIONS ENVIRONMENTAL TEST SPECIFICATIONS RTCA DO 160B ENV CAT Temp and Altitude Low Operating Temp High Operating Temp High Short Op Temp Low Survival Temp High Survival Temp Altitude Decompression Overpressure Temp Variation Humidity Vibration Shock CHARACTERISTICS C1BA SLM XXXXXXZBBXXXX Category C1 20 deg 55 deg 70 deg 55 deg 85 deg 00o0oD0OoO 35 000 ft Equipment mounted in Pressurized or Non Pressurized cabin area 15 000 ft Category B Internal section of aircraft 2 deg C minimum per minute Category A Standard humidity of 50 deg C at 95 RH reduced to 38 deg C 48 hours exposure Categories SLM Equipment mounted on equipment rack or fuselage or inst panel for fixed wing turbojet reciprocating turbopropeller turbojet engine aircraft Half sine wave 6 Gn total duration of 11 2 msec INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 SPECIFICATIONS Magnetic Effect Power Input Voltage Spike CHARACTERISTICS Category Z 21 Catefory B Equipment for use on aircraft electrical systems supplied by engine driven alternator rectifiers or DC generators where battery is floating on the DC bus at all times
23. ge B4 ci fai eh flan c cz fiz C2 Brown c2 ca 112 C4 Violet c4 Strobe t Strobe Pink Strobe DC Ground 15 DC Ground Black DC Ground Power Input 14 28 Vde Red 14 28 Vde AK 350 With Strobe Type ALTITUDE REPORTER ATC TRANSPONDER Figure 2 2A Connector Pin Function intertace with Strobe type ATC Transponder Not Connected D2 D2 D4 D4 Ai AI White Ri YA A2 Gray Re AA A4 Blue A4 Bi B1 Green B1 B2 B2 Yellow B2 84 fio L B4 Orange B4 ci c1 Tan ci c2 C2 Brown c2 c4 12 H EL Violet C4 Strobe Strobe Pink Strobe DC Ground 15 2E Ground Block DC Ground Power Input 14 28 Vdc Red 14 28 Vde AK 350 Without Strobe Type ALTITUDE REPORTER ATC TRANSPONDER Figure 2 3A Connector Pin Function interface with Non Strobe type ATC Transponder NOTES Connection required for 35 000 ft 40 000 ft 50 000 ft 62 000 ft amp 80 000 ft Configurations only Connection required for 80 000 ft Configuration only 8A INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 360 DC Ground Black 14 28 Vdc Switched Power 14 Vde Red or 28 Vde Power Input AK 350 ALTITUDE REPORTER ATC TRANSPONDER Figure 2 4 Power pins interface with Switched power output type Transponder All wires are 22 AWG DC Ground Black Xponder DC Ground DC Ground 14 28 Vdc Non Switched 14 V
24. ges or modifications Service Bulletins The present authorization is limited to components imported and identified with applicable TSO markings as approved by the FAA Beme 4 March 1993 Section for Type Certifications YA b o John D tsch 33
25. lor t A1 u 2 White A2 13 Gray _ AA 4 Blue Bi 15 Green B2 _ 19 Yellow 10 Orange 111 Tan Bm Wht 113 Brown 112 ViolevPurple Biue 4 Lt Green Note 1 147 Blk Wht Note 2 DC Power In 8 Red DC Ground 115 Black No Connection 14 Red Wht MARES L N J Note 2 No Connection Leave Pin Open for PIN AK 350 AK 35035 AK 35040 AK 35050 AK 35060 This Connection is required for P N AK 35080 only ne 1 No Connection Leave Pin Open for P N AK 350 This Connection is required for P N AK 35035 AK 35040 AK 35050 AK 35060 amp AK 35080 only General Note It is getan that Refer to Tran nsponder Manufacturer Installation Manual for Actual Installation FIGURE 2 11 ALTITUDE ENCODER INTERCONNECT Bea DIAGRAM WITH STROBED TRANSPONDERA tT T ua De _ ie 38OULS NON HUM INVYOVIO SUWWaHos LI3NNOJU3LNI Y3009N3 JONA TW oz ETIOPIE FR UORBIBISU 8nJ9Y 10 BNUBN UORE EJSU Jepucdsuas 0 Jejey Je nena a SH OJON jeleuss yani juo OBOSE AV Y 090SE NV 0S05531V Or0SE NV SEOSESIV Nid Jo peunbey sy UORISUUOI SIUL T OS NV N d 10 uedo Uid ABET UORDBUUOS ON LON 1 Kuo 080SE MY Nid 40 Pennbai s vopseuuog Sy PUE OSOSE HY OPOSE MV SEOSEAV OSE NV Nid 10 ued6 uid eAB87 UORSEULIOD ON Z B
26. n ee ee CO BCAA MINAS EIN ai EIN MO za AE No on EROS ON TaN WR pa Be wm O 200 po BI en oT ee oe ze IT I Te TB LH Tem 9 Ber a eg Du Be RE re ee a 3 Poe AD NA Fang Be zer O E SA ee ee gee TEA E Se ee le Wa Ei oe ee CARDO E onu oaa oa B penen 12 18 aN j E ws aa ana aa ae AA ________ ers comm GPS RNAV GPS RNAV GPS NAV GPS GNCIGNIGPSIGNCION GPs nav ALT ENCODER AMERI KING Honeywell Honeywell Honeywell Honeyweil Garmin Garmin Trimble SIGNAL AK 350 kux 135 135a KLN 898 94 KLN90B KLN 900 140014201430 2000 FUNCTION pin No Wire Color PinNo Ps92 Poo P9001 P4001 P5001 Pa T AA E SAMA Y a ee ate ee ae IA ie E A1 ame te ae a oe 1 31 11 Az Jhay M 2 3 a 35 68 68 14 AA 1m ar 20 a a er Te YT 20 B1 S Grem 10 25 17 6 66 15 77 82 o vYelow 18 26 54 6 65 3 1 B4 tO Orange 17 27 47 58 64 64 318 1 et f1 Tan Brnwht 44 28 48 as dT 68 4 C2 OL 3 Brown 13 29 49 18 62 6 77 17 C4 I12 violevPupierne 12 30 50 4 61 61 15 77 Da 1 tGreen Note 1 6 Note 1 21 Note 1 41 Note 1 13 Note 1 70 Note 1 70 Note 1 13 Note 13 D2 7 Bkwmnote2 No Connect No Connect Strobe DC Grouna 6 Pink DcGnd pcGnd DCGnd DcGnd 160 DC Gnd 60 DC Gnd 18 DC Gnd a DC Power In 8 Red DC Power
27. on while awaiting quality control approval Subj Request for LBA Approval for Altitude Encoder AK 350 of that facility Ref Your application dated June 22 1992 Enels 1 Type Certificate Sincerely 1 Technical Data Sheet 1 Bill of Costs e hehe AR Frederick Lee Manager Los Angeles Aircraft Dear Sirs Certification Office This letter is to notify you that the Altitude Encoder AK 350 designed and manufactured by Ameri King Corp has received type approval The Type Certificate No 10 221 6 is issued on the basis of the pertinent rules in the German Aviation Act and paragraph 4 of the Certification Regulations as in force today The type approval is valid as determined in the associated Technical Data Sheet No 10 221 6 issue 1 The technical data sheet can be obtained from Verlag R Eisenschmidt GmbH Frankenallee 25 6000 Frankfurt Main after printing The type approval wili be promulgated in the Nachrichten f r Luftfahrer In compliance with paragraph 5 of the Certification Regulations this office must be notified of any minor or major design change by the manufacturer Dienstgeb ude Telefon 0531 2355 0 Bundeskasse Postgiroamt Landeszentraibank 29 Braunschweig Telex 952701 LRA Hannover Hannover Hannever INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Ameri King Corp is committed to supply to this office all future revision sheets to the Installation Manual Service Bulletins and other pertinent
28. ot possible If the aircraft ceiling altitude is less than 30 000 feet perform the same above procedure for its ceiling altitude i e for a maximum aircraft operating altitude of 20 000 feet the flight altimeter shall indicate 19 950 20 feet at the transition point 19 900 20 000 feet 20 2 6 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Step 5 Step 6 Step 7 Apply static pressure system tester to obtain a flight altimeter reading of 100 feet Slowly increase pressure and read the flight altimeter at transition point 100 O feet Transition point is indicated on the Transponder Test Set If necessary adjust the LO pot of the AK 350 until the transition point at increasing pressure is 50 10 feet as read on the primary flight altimeter Check the transition points at flight altitude reading of 30 000 feet for both decreasing and increasing pressure The transition point for decreasing pressure should be 29 950 50 feet The transition point for increasing pressure should be 30 050 50 feet Check the transition points at flight altitude reading of O feet for both decreasing and increasing pressure The transition point for increasing pressure should be 50 50 feet The transition point for decreasing pressure should be 50 50 feet Repeat the above procedures until interaction is eliminated DATA CORRESPONDENCE TEST Reference FAR 91 36
29. r DC Power DC Power DC Power DC Ground _ 15 Black TT 1310c Gna 206 ana 24 DC Gnd DC Ground DC Ground DC Ground DC Ground No Connection 14 Red Wht No Connect No Connect No Connect No Connect No Connect No Connect No Connect RUI mate Y E a fee ee ee rer A e 2 No Connection Leave Pin Open for P N AK 350 meet AK 35040 ee __ Note 1 No Connection Leave Pin Open for P N AK 350 en MAA T This Connection is required for P N AK 35035 AK 35040 AK 35050 AK 35060 amp AK 35080 only _ General Note it is important that Refer to Transponder Manufacturer Installation Manual for Actual Installation JE ee Y AN FRE HS DIET DATO HE i FIGURE 2 6 ALTITUDE ENCODER INTERCONNECT SCHEMATIC DIAGRAM WITH NON STROBE TRANSPONDERS 3 ESPN 7 DEFI a eee EA SURONOASNVHL 038015 HAM AVEOVIO DILVAIHOS LOaNNOOUSINI USOODNA SONI LE UND B UONBIBISUL JENIOY 104 jenueyy LONBIE SU JeJmoe nuByy JepuodsuBJ 0 18504 eU weuodun 0J0N B 10U0 INEA NA HN O IUO O8OSE AV 8 O90SE AV OSOGE NV OPOSEDAV SEOSE HV N d 0 pesinbel si UONISUUO SUL DEE PS AA ES Bee EAS ZEN OSE MV N d 40 uedo Uld BABET UONSBUUOD ON BION Auo OBOSE AV Nid 10 pesinbel s UOOeUUOD SIUL E a ErIV OSOS SEOSE MV OSE AV N d 104 UedO Uld BABET UONOBUUOD ON Z ee BEE ao a mes Fe WEE onsen isa bere Sif puros aa AO oa teresa masa BAA SAI BA Tai Ber
30. tic system will make calibration and data correspondence test difficult if not possible If the altimeter correspondence error exceeds 125 ft flight altimeter calibration should be suspected 22 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 Correspondence Transition for Transition for Test Point Decreasing Pressure Increasing Pressure 1 000 ft 1 050 125 ft 950 125 ft O ft 50 125 ft 50 125 ft 2 000 ft 1 950 125 ft 2 050 125 ft 6 000 ft 5 950 125 ft 6 050 125 ft 10 000 ft 9 950 125 ft 10 050 125 ft 14 000 ft 13 950 125 ft 14 050 125 ft 20 000 ft 19 950 125 ft 20 050 125 ft 25 000 ft 24 950 125 ft 25 050 125 ft 30 000 ft 29 950 125 ft 30 050 125 ft 35 000 ft 34 950 125 ft 35 050 125 ft 40 000 ft 39 950 125 ft 40 050 125 ft 50 000 ft 49 950 125 ft 50 050 125 ft 60 000 ft 59 950 125 ft 60 050 125 ft 70 000 ft 69 950 125 ft 70 050 125 ft 80 000 ft 79 950 125 ft 80 050 125 ft Maximum Correspondence Error shall be 125 feet as read on the primary flight altimeter NOTE 1 If the aircraft ceiling altitude is less than 80 000 feet perform the same above procedure for its ceiling altitude i e from 1 000 feet to maximum aircraft ceiling altitude Because mechanical primary flight altimeter pointers are not totally frictionless therefore tap lightly on the primary flight al
31. timeter with a screwdriver handle to eliminate friction before taking any reading A leaky static system will make calibration and data correspondence test difficult if not possible If the altimeter correspondence error exceeds 125 ft flight altimeter calibration should be suspected 224A INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 2 7 PLACARDING The altimeter used for flight reference and the Mode AK 350 shall be placarded the following information 3 1 Placard is included with the Installation Kit Replacement or re calibration of the altimeter used for flight reference requires re calibration of Model AK 350 Altitude Reporter 3 2 Altitude encoded to feet 23 INSTALLATION MANUAL ALTITUDE REPORTER ENCODER MODEL AK 350 SECTION Ili OPERATION GENERAL This section describes the operation of the AK 350 Altitude Reporter Altitude Encoder OPERATION The AK 350 Altitude Reporter is an integrated circuit technology based equipment It is a highest standards of quality and extremely reliable equipment equipment rack mounted designed to meet TSO C88a requirements The AK 350 Altitude Reporter is connected to the aircraft pneumatic static system and output to the ATC Transponder It converts altitude pressure into altitude digital data output to ATC Transponder When the ground station requests for reporting the altitude the Transponder will transmit the altitude digital
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