BXP R-(XX) Class 1. BXP R-(XX) Class 2

Transcription

1 NSCM: D2356 Remote controlled Transponder BXP R-(XX) Class 1 BXP R-(XX) Class 2 ATC Mode S / Le vel 2 es INSTALLATION AND OPERATION Manual DV PN Be cker Flugfunkwerk GmbH Baden-Airpark B Rhein müns ter Ger ma ny Telephone +49 (0) 7229 / Fax +49 (0) 7229 / cker-avionics.de info@becker-avionics.de or support@becker-avionics.de Initial Issue: December February 2007

2 Copyright by Be cker Flugfunkwerk GmbH Rheinmünster Germany All rights reserved. Subject to technical changes.

3 RE CORD OF RE VI SIONS REV. NO. IS SUE DATE IN SER TED REV. NO. IS SUE DATE IN SER TED DATE BY DATE BY 1 February /07 Becker ROR Page February 2007

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5 IN STAL LA TI ON AND OPE RA TI ON LIST OF EF FEC TI VE PA GES SUB JECT PAGE DATE SUB JECT PAGE DATE Tit le Page TP-1 Feb TP Record of Revisions ROR-1 Feb ROR-2 blank List of Effective Pages LEP-1 Feb LEP-2 blank Introduction Intro-1 Dec Intro-2 Dec Intro-3 Dec Intro-4 blank Table of Contents I-I Dec I-II blank General Description 1-1 Feb Dec Dec Dec Dec Feb Feb blank Table of Contents II-I Dec II-II blank Installation 2-1 Feb Dec Feb Dec Dec Dec Feb Dec Dec Dec Dec Dec Dec blank LEP Page February 2007

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7 IN TRO DUC TI ON 1. Gen eral The re mo te con trol led Mode S trans pon der is des cri bed in this ma nu al Installation and Operation. 2. Manufacturer The re mo te con trol led Mode S trans pon der was de ve lo ped and is ma nu fac tur ed by: Be cker Flug funk werk GmbH Ba den-airpark B Rhein müns ter / Germany Te le pho ne: +49 (0) 7229 / Te le fax: +49 (0) 7229 / cker-avionics.de info@be cker-avionics.de or sup port@be cker-avionics.de CER TI FIED QUA LI TY SYS TEM The Be cker qua li ty ma na ge ment sys tem is cer ti fied ac cor ding to : DIN EN ISO 9001:2000 CERT Reg. - Nr LI CEN SES AND AP PRO VALS DE.21G.0075 Ap pro val as ma nu fac tu rer to EASA PART 21 DE Ap pro val as main ten an ce or gani za ti on to EASA PART Sa fe ty information The installation of the Mode S transponder into an aircraft may be carried out only by an authorized installation company. The country regulations always have to be observed. Do not con nect the unit to AC sour ces. Make sure that the unit is con nec ted to a DC sour ce 33 V DC. The unit should be pro tec ted from the air craft po wer supp ly by a de di ca ted 5 A cir cuit brea ker for class 1 and 3 A for class 2. Do not con nect the unit with re ver sed po la ri ty to the DC sour ce. Do not switch on the unit be fo re the air craft engines are started. Switch off the unit be fo re the en gi nes are shut down. Do not ope ra te the unit un der am bient tem pe ra tu res be low -40 C for class 1 or -20 c for class 2 and abo ve + 70 C. IN TRO Page 1

8 Voltages > 42 V are possible within the transponder. The programming of the address module AM with the ICAO 24-bit address of the aircraft must be carried out only at an installation company or in the manfacturer factory. 4. Lay out of manual The ma nu al is divi ded into two chap ters: - GE NE RAL DES CRIP TI ON - IN STAL LA TI ON 5. Re vi sions of the manual All chan ges to the ma nu al are re cor ded con se cu ti ve ly on the pre-page Record of Revi sions. 6. List of ab bre via tions AA ADLP AI ALT ATC BIT CBIT DV EASA ELS EHS es FAA FL FMS FN GICB GND ICAO IBIT ID IDT IFR MTL NSCM ON PBIT PN RX Ai craft Ad dress (24-bit ICAO) Avio nics Data Link Processor Air craft Iden ti fier Al ti tu de or trans pon der ALT mode Air Traf fic Con trol Built-In Test Con ti nu ous Built-In Test Manual identification number Eu ro pe an Avia ti on Sa fe ty Agen cy Ele men ta ry Sur veil lan ce En han ced Sur veil lan ce e = Extended squit ter and s = SI capability Fe de ral Avia ti on Ad mi nis tra ti on Flight Level Flight Ma na ge ment System Flight Number Ground Ini tia ted Comm-B Ground In ter na tio nal Ci vil Avia ti on Or gani za ti on In itia ted Built-In Test Iden ti fier Ident (Iden ti fi ca ti on) In stru ment Flight Rules Mi ni mum Trig ge ring Level Nato Supp ly Code of Manufacturers Transponder ON mode (without altitude transmission) Power-on Built-In Test Part Number Receiver IN TRO Page 2

9 SBY SEL SI SPI STO SUPP TIS TX VFR XPDR Stand by mode Se lec ti on Sur veil lan ce Iden ti fier Spe ci al Po si ti on Iden ti fi ca ti on Pulse Sto re Supply voltage DC Traf fic In for ma ti on Ser vi ce Transmitter Vi su al Flight Ru les Transponder IN TRO Page 3

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11 TAB LE OF CON TENTS GE NE RAL DES CRIP TI ON Page 1. Ap pli ca ti on Ge ne ral des crip ti on Tech ni cal data Soft wa re Sys tem ap pro vals Equipment Ac ces so ries 1-6 Page I-I

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13 GE NE RAL DES CRIP TI ON 1. Ap pli ca ti on The re mo te con trol led Mode S trans pon der forms, to get her with the cor re spon ding con trol unit, the air bor ne com po nent of the Air Traf fic Con trol (ATC). It functions in ac cor dan ce with the se con da ry ra dar prin ci ple and al lows air traf fic con trol to lo ca te, iden ti fy and track air craft. 2. Ge ne ral des crip ti on A. The is a re mo te con trol led unit de sig ned for in stal la ti on in the avi onic com part ment of air craft. B. The two 25-pin unit con nec tors for con nec ti on to the air craft in ter wi ring, the 5-pin sub mi nia ture con nec tor for the Ad dress Mo du le AM (XX) and the TNC an ten na socket are lo ca ted at one side of the unit. C. A seri al in ter face RS-422 for con nec ti on of the con trol unit is avai lable at the unit con nec tor. All con trol ele ments are lo ca ted on the front pa nel of the correspon ding con trol unit CU (XX). Ins te ad of the CU (XX), the trans pon der may also be con trol led by anot her de vi ce (e.g. ADLP) via the con trol in ter fa ce. D. The re mo te con trol led trans pon der provides the fol lo wing fea tu res: (1) In the selective mode (Mode S), the Ground Con trol can inter ro ga te the trans pon der in di vi du al ly using an ICAO-24-bit ad dress, which is uni que to the par ti cu lar air craft. (2) Sup port of the SI code (Sur veil lan ce Iden ti fier) (3) Regis ter ca pa bi li ty for el emen ta ry sur veil lan ce (ELS) and en han ced surveil la nce (EHS) (4) Exten ded squit ters trans mis si on. (5) Data link ca pabi li ty E. Inherent features: (1) Mode A - in this mode, the 4096 cha rac ter code set on the con trol in ter fa ce is sent as a reply to in ter ro ga ti on from a ground sta ti on. (2) Mode C - in this mode, the en co ded altitude is sent in ad di ti on to the mode A reply. The alt itu de in for ma ti on must be de li ver ed from an ex ternal device (e.g. Becker Blind Encoder BE6400). (3) A spe ci al iden ti fier pul se (SPI) can be ac ti vat ed by the con trol in ter fa ce or ex ter nal push-button in Mode A/C and Mode S. (4) Self tests (BITs). The Ini tia ted Built-In Test (IBIT), the Con ti nu ous Built- In Test (CBIT) and the Power-on Built-In Test (PBIT) are in te gra ted in the trans pon der. Page February 2007

14 3. Tech ni cal data A. Ge ne ral data Supp ly vol ta ge Typical con sump ti on Se ri al in ter fa ces Data link ca pa bi li ty 10.0 V to 33.0 V DC 50 mode S replies/sec. + squit ter 0.35 A at 14 V 0.20 A at 28 V in stand by mode: 0.18 A at 14 V 0.13 A at 28 V RS GICB re gis ters DME sup pres si on: - in put vol ta ge < 2 V (no sup pres si on) > 8 V (sup pres si on) - out put vol ta ge < 0.5 V (not ac ti ve) > 18 V (ac ti ve) Ex ter nal Ident in put: 0 (ac ti ve) 3.5 V 1 (pas si ve) 4.0 V Isour ce (shor ted to GND) 10 ma Ground de tec ti on in put: ground air bor ne Isour ce (shor ted to GND) Po wer-up time In ter nal fuse pro tec ti on 0.5 V 2 V 10 ma 2 s (in clu ding in ter nal self-test) F 5 A Ex ter nal fuse pro tec ti on 5 A (class 1) 3 A (class 2) Ope ra ting tem pe ra tu re ran ge - 40 C to + 55 C (class 1) - 20 C to + 55 C (class 2) (short-time + 70 C) Sto ra ge tem pe ra tu re ran ge - 55 C to + 85 C Ope ra ting al ti tu de ft. max. (class 1) ft. max. (class 2) Mode S Con for mi ty Class 1or 2, Le vel 2 es - ex ten ded squit ter capability - sur veil lan ce iden ti fier (SI code) RTCA DO-181C FAA TSO-C112, class 2a Eu ro cae ED-73B, le vel 2es, class 1 or 2 EASA ET SO-2C112a Page 1-2

15 En vi ron men tal con di tions (see also pa ra graph D) in ac cor dan ce with EU RO CAE/ RTCA ED-14D/DO-160D Me cha ni cal di men sions : - Front plate 61 x 61 mm (H x W) (2.401 x inch) - Case depth with an ten na so cket 184 mm (7.244 inch) - Case depth with ad dress mo du le 215 mm (8.464 inch) Weight ap prox kg (1.499 lb) B. Re cei ver data Ope ra ting mo des Re cei ve fre quen cy Sen si ti vi ty (MTL) Se lec ti vi ty Dy na mic ran ge Band width Mo du la ti on (mode A/C) Mo du la ti on (mode S) Side lobe sup pres si on No mi nal im pe dan ce Mode A/C/S, depen ding on interrogation 1030 MHz ± 0.1 MHz (mode A/C) 1030 MHz ± 0.01 MHz (mode S) - 74 dbm ± 3 db (for 90 % re ply rate in mode A/C and 99 % in mode S) ± 15 MHz > 40 db ± 25 MHz > 60 db 60 db ± 3 MHz < 3 db PAM (Pul se Am pli tu de Mo du la ti on) DPSK (Dif fe ren ti al Phase Shift Key ing) 3-pulse me thod (mode A/C) P5 (mode S) 50 Ω C. Trans mit ter data Trans mit fre quen cy Trans mit mo du la ti on Trans mit ter type Trans mit po wer (class 1) 1090 MHz ± 1 MHz 12MOM1D PAM (Pul se Am pli tu de Mo du la ti on) So lid sta te 125 W (+ 21dBW) at an ten na end ter mi nal and 250 W at unit out put Page 1-3

16 Trans mit po wer (class 2) Re ply rate ca pa bi li ty (mode A/C) Re ply rate ca pa bi li ty (mode S) Mode S squit ter rate (ap prox.) 70 W (+18.5 dbw) at an ten na end terminal and 140 W at unit output at least 1200 mode A/C replies per se cond for a 15 pul se coded reply, can be li mit ed to at least 50 mode S re plies in one-second in ter val (the re of at Least 16 long for mats) Ac qui si ti on squitter 4/sec. Ex ten ded squitter 1/sec. Re ply code (mode A) ICAO co ding sys tem with 4096 pulse re ply pos si bi li ties (octal code) Altitude code (mode C) Al ti tu de code (mode S) Trans mit pul se sha pe No mi nal out put im pe dan ce ICAO coding system 100-ft. Steps from to ft. 25 ft. or 100 ft. steps (de pen ding on sour ce) pul se width 0.45µs ± 0.1µs (mode A/C) pul se width 0.5µs ± 0.05µs (mode S) rise time 0.05 to 0.1µs fall time 0.05 to 0.2µs 50 Ω D. En vi ron men tal con di tions in ac cor dan ce with EU RO CAE/RTCA ED-14D/DO-160D In put vol ta ge ran ge 10.0 to 33.0 V DC Low ope ra ting tem pe ra tu re -40 C for class 1 or -20 C for class 2 High ope ra ting tem pe ra tu re High short-time ope ra ting tem pe ra tu re Sto ra ge tem pe ra tu re ran ge In-flight loss of coo ling Al ti tu de Hu mi di ty Vi brat ion re sis tan ce Ope ra tio nal shocks + 55 C + 70 C - 55 C to + 85 C Cat. Z, no au xi lia ry coo ling re qui red ft. max. Cat. A / + 50 C; 95%, 48 h Cat. S, test cur ve M Cat, U, test cur ve G 6 g in any di rec ti on Page 1-4

17 Crash sa fe ty Mag ne tic ef fect En vi ron men tal ca te go ries: 20 g shocks 20 g ac cele ra ti on Ca te go ry Z Env.Cat. [D1Z] BAB[(SM)(UG)]XXXXXXZBA BA[WW]B[A3E3X] XXA E. En vi ron men tal qua li fi ca ti on EU RO CAE/RTCA ED-14D/DO-160D Con di ti on Sec ti on Cat. Des crip ti on Tem pe ra tu re and Al ti tu de 4.0 D1 Equip ment tes ted to Ca te go ry D1 Low Ground Sur vi val Tem pe ra tu re D1-55 deg C Low Ope ra ting Tem pe ra tu re D1 BXP R-(XX): -40 deg C High Ground Sur vi val Temp D1 +85 deg C High Short-Time Ope ra ting Temp D1 +70 deg C High Ope ra ting Temp D1 +55 deg C In-flight Loss of Coo ling Z No for ced coo ling re qui red No test re qui red Al ti tu de D1 A1 BXP R-(XX): ft (class1) BXP R-(XX): ft (class 2) De com pres si on Not applicable Over pres su re Not appli ca ble Tem pe ra tu re Va ria ti on 5.0 B Equip ment tes ted to Ca te go ry B Hu mi di ty 6.0 A Equip ment tes ted to Ca te go ry A Shock and Crash Sa fe ty 7.0 B Equip ment tes ted to Ca te go ry B Vi brat ion 8.0 S U Cat. S, vi brat ion test cur ve M Cat. U, vi brat ion test cur ve G Ex plo si on Pro of ness 9.0 X No test re qui red, Equip ment iden ti fied as Cate go ry X Wa ter pro of ness 10.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Fluids Sus cep ti bi li ty 11.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Sand and Dust 12.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Fun gus Re sis tan ce 13.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Salt Spray 14.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Mag ne tic Ef fect 15.0 Z Equip ment is Class Z Po wer In put 16.0 B Equip ment tes ted to Ca te go ry B Vol ta ge Spi ke 17.0 A Equip ment tes ted to Ca te go ry A Au dio Freq. Con duc ted Sus cep ti B Equip ment tes ted to Ca te go ry B bi li ty In du ced Sig nal Sus cep ti bi li ty 19.0 A Equip ment tes ted to Ca te go ry A Ra dio Fre quen cy Sus cep ti bi li ty 20.0 WW Equip ment tes ted to Ca te go ry WW Spu ri ous RF Emis si on 21.0 B Equip ment tes ted to Ca te go ry B Light ning In du ced Tran sients Sus A3E3X Equip ment tes ted to Ca te go ry A3E3X cep ti bi li ty Light ning Di rect Ef fects 23.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Icing 24.0 X No test re qui red, Equip ment iden ti fied as Ca te go ry X Elec tro sta tic Disch ar ge 25.0 A Equip ment tes ted to Ca te go ry A Page 1-5

18 4. Soft wa re The re mo te trans pon der BPX 6402-XR-(XX) is con trol led by a microcontroller.the soft wa re cri ti ca li ty is de ter min ed to be Le vel C in ac cor dan ce with EUROCAE/ RTCA do cu ment ED12B/DO-178B. 5. Sys tem ap pro vals EASA FAA ETSO-2C112a TSO-C Equipment BXP R-(01) Remote Transponder, Article-No Level 2, class 1 BXP R-(01) Remote Transponder, Article-No Level 2, class 2 AM (01) Address Module Article-No MK 4401 Mounting kit Article-No BE (01) Blind Encoder Article-No Ac ces so ries AMP Ad dress Mo du le pro gram mer Ar ti cle-no kit (soft wa re and ca ble), par al lel in ter fa ce CK 4401-C Stan dard con nec tor kit Ar ti cle-no D-Sub plug, 25-pin (crimp ver si on) CK 4401-S Stan dard con nec tor kit Ar ti cle-no D-Sub plug, 25 pin (sol de ring ver si on) CK 6400-C Ex ten ded con nec tor kit Ar ti cle-no D-Sub plug, 25-pin 1 D-Sub jack, 25-pin (crimp ver si on) CK 6400-S Ex ten ded con nec tor kit Ar ti cle-no D-Sub plug, 25-pin 1 D-Sub jack, 25-pin (sol de ring ver si on) TNC coa xi al con nec tor for RG-58C/U Ar ti cle-no (crimp ver si on) TNC coa xi al con nec tor for RG-223/U Ar ti cle-no (crimp ver si on) Page February 2007

19 TNC coa xi al con nec tor for RG-58C/U Ar ti cle-no and RG-223/U (sol de ring ver si on) or spa re con nec tor Ar ti cle-no A032 Trans pon der rod an ten na Ar ti cle-no Coa xi al con nec tors for an ten na 1A032: BNC an ten na con nec tor for RG-58C/U (crimp) Ar ti cle-no BNC an ten na con nec tor for RG-223/U (crimp) Ar ti cle-no BNC an ten na con nec tor for RG-58C/U and RG-223/U (sol dering) Ar ti cle-no Ma nu als: INSTALLATION AND OPERATION In stal la ti on and Operation Article-No Maintenance and Repair Article-No Control Interface Protocol Article-No Data Transfer Interface Protocol Article-No BXP 640X-XX-(XX) Installation and Operation BE (XX) Article-No Page February 2007

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21 TAB LE OF CON TENTS IN STAL LA TI ON Page 1. Ge ne ral In spec ti on be fo re in stal la ti on Me cha ni cal in stal la ti on Air craft wi ring In stal ling the trans pon der an ten nas 1A Pro gram ming of the Ad dress Mo du le Avio nics data transfer Remo te con trol Set tings af ter in stal la ti on Chec king af ter in stal la ti on 2-8 Fig. 2-1 In stal la ti on di men sions, mea su res in mm 2-9 Fig. 2-2 Moun ting instal la ti on di men sions, mea su res in mm 2-10 Fig. 2-3 In stal la ti on di men sions 1A Fig. 2-4 Pro po sal for air craft wi ring 2-12 Fig. 2-5 RS-232 seri al en co ding al ti me ter con nec ti on 2-13 Page II-I Decmber 2005

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23 IN STAL LA TI ON 1. Ge ne ral In stal la ti on of the re mo te con trol led trans pon der is de pen ding on the air craft type and its clas si fi ca ti on as well as re qui re ments. The re fo re, only ge ne ral in for ma ti on can be pro vi ded in this sec ti on. 2. In spec ti on be fo re in stal la ti on Be fo re the trans pon der is in stal led on an air craft, a vi su al in spec ti on for pos si ble trans port da ma ges shall be done. Please look for the following defects: (1) Dirt, dents, scratches, corrosion, broken fastening elements on housing and housing parts. (2) Dirt and scratches on nameplate and inscriptions. (3) Dirt, bent or broken pins, cracked insert of unit connector and antenna socket. (4) Missing screws. 3. Me cha ni cal in stal la ti on The re mo te con trol led trans pon der is to be fit ted at a suit ab le pla ce on the air craft. This is usu al ly the avio nics com part ment. The moun ting pla ce shall be at least 30 cm from the mag ne tic air craft com pass, to avoid any in ter fe ren ce to the mag ne tic com pass by the trans pon der.the ne ces sa ry di men sions for the in stal la ti on are gi ven in Fig. 2-1 and Fig First se cu re the unit moun ting using three coun ter sunk screws and then sli de the trans pon der into the moun ting and lock in pos iti on. Blind Encoder installation: For installation of the Becker Blind Encoder BE6400 the corresponding manual (Article- No ) has to be noticed. The Blind Encoder BE6400 is intended to be connected to the J8 unit connector of the transponder and can be used only in installations that do not require connection of other equipment utilizing ADLP interface of the transponder.the Blind Encoder is direct connected to the transponder, without any interwiring. CAUTION : Becker takes a guarantee for the equipment only, if the transponder is installed with the mounting, which is mentioned in this manual (MK 4401 mounting kit, Part No ). 4. Air craft wi ring A. The air craft wi ring of the trans pon der is shown in Fig CAU TI ON : For in stal la tions in a more se ve re elec tro mag ne ti cal en vi ronment use shiel ded ca ble con nec tors and a com mon shiel ding for the transpon der in ter wi ring. Page February 2007

24 B. RF con nec tor The unit RF con nec tor is of the TNC fe ma le type. The an ten na ca ble shall be of low-loss 50 Ω ca ble, at least RG 58C/U or bet ter RG 223/U type. Pin Name Pin Des crip ti on Sour ce Des ti na ti on Re com men ded cable type An ten na 50 Ω TNC an ten na con - bi-directional to the bi-directional to the RG58C/U or nec tor, fe ma le an ten na an ten na RG223/U C. Pin con nec tions of the unit con nec tor P9 The unit con nec tor type is D-SUB 25-pole male. Pin Pin Name Pin Des crip ti on Sour ce Des ti na ti on Re com men - ded cable type A1 A2 A4 Al ti tu de A1 Al ti tu de A2 Al ti tu de A4 En co ding al ti me ter (paral lel in ter fa ce) BXP 6402-XR 3xAWG24 13 GND DC supp ly Ground, ad di tio nal con nec ted to Pin IDENT_N Ident but ton, ext. Ex ter nal Ident BXP 6402-XR AWG26 but ton 5 EXT. SUP- PRESSION Aircraft sup pres si on system bi-directional bi-directional Coaxi al cable 6 SWIT CHED Swit ched supp ly vol ta - BXP 6402-XR En co ding al ti me ter PO WER OUT ge I max = 1 A 7 RE PLY OUT Out put for ext. re ply BXP 6402-XR Re ply lamp AWG26 lamp, lamp to be con - nec ted to po si ti ve il lu - mi na tion vol ta ge 8 9 RX+ RX- RS-422 data inter fa ce CU BXP 6402-XR 2xAWG26, shielded SUPP Supp ly vol ta ge in put, ex ter nal 5 A fuse for cur rent pro tec ti on DC supp ly vol ta ge sour ce 10 to 33 V BXP 6402-XR 2xAWG20 B1 B2 B4 C1 C2 C4 D4 TX+ TX- Al ti tu de B1 Al ti tu de B2 Al ti tu de B4 Al ti tu de C1 Al ti tu de C2 Al ti tu de C4 Al ti tu de D4 DC supp ly vol ta ge Ground En co ding al ti me ter (paral lel in ter fa ce) BXP 6402-XR BXP 6402-XR AWG20 7xAWG24 RS-422 data interface BXP 6402-XR CU xAWG26, shielded 24 ON_N ON/OFF sig nal CU BXP 6402-XR AWG26 25 GND Ground, ad di tio nal con nec ted to Pin 13 DC supp ly vol ta ge Ground BX6402-XR AWG20 Page 2-2

25 D. Pin con nec tions of the unit con nec tor J8 The unit con nec tor type is D-SUB 25-pole female Pin Pin Name Pin Des crip ti on Sour ce Des ti na ti on Re com men - ded cable type 1 PSEL Protocol selection DC supply voltage BXP 6402-XR AWG26 ground 2 Not connected Reserved for GPIN1 3 GND Ground connection 4 BSUPP Supply for BE6400* BXP 6402-XR BE Not connected 6 Not connected Re ser ved for GPSRX- 7 Not connected Re ser ved for GPSRX+ 8 Not connected Re ser ved for hi jack mode (HI) 9 Not connected Re ser ved for hi jack mode (HO) 10 Not connected Re ser ved for SQ 11 GND SWITCH Weigth on wheel Aircraft BXP 6402-XR AWG26 sensor ALTS- ALTS+ RS-422** data interface Se ri al enco ding altimeter BXP 6402-XR AWG26 shielded TISRX- TISRX+ 16 Not connected 17 TISTX- 18 TISTX+ RS-422 data interface 19 Not connected 20 Not connected 21 GND Ground connection 22 Not connected 23 Not connected 24 Not connected 25 Not connected Avio nics Data Link Pro ces sor BXP 6402-XR RS-422 data interface BXP 6402-XR Avio nics Data Link Pro ces sor * NOTE: Do not connect if no BE6400 is used. ** NOTE: See Fig. 2-4 for RS-232 serial encoding altimeter connection. 2xAWG26 twis ted pair, shiel ded all together 2xAWG26 twis ted pair, shiel ded all together E. Pin con nec tions of the unit con nec tor J7 The unit con nec tor type is sub mi na tu re 5-po le fe ma le. Pin Pin Name Pin Des crip ti on Sour ce Des ti na ti on 1 VCC Po wer supply BXP 6402-XR AM (01) 2 I 2 C_CLK Clock AM (01) BXP 6402-XR 3 Not con nec ted Reserved 4 I 2 C_DAT Data AM (01) BXP 6402-XR 5 GND Po wer supp ly return BXP 6402-XR AM (01) Page February 2007

26 F. DME sup pres si on If re qui red, con nect the sup pres si on in/out of trans pon der to the cor re spon - ding pin of the DME unit or any rel evant de vi ce. G. Ex ter nal IDENT push-button If this in put (Pin 4 of unit con nec tor P9) is brief ly con nec ted to GND (e.g. by an ex ter nal push-button), the IDENT functi on (SPI) is start ed in the same way as when using the IDENT push-button on the front pa nel. H. Ground switch If re qui red, con nect an au to ma tic ground switch (weight on wheel sen sor) at Pin 11 of unit con nec tor J8. 5. In stal ling the trans pon der an ten na 1A032 A. The trans pon der an ten na has to be fit ted to the bottom of the air craft at a ho rizon tal, flat lo ca ti on. This lo ca ti on should not be in the sha dow of air craft struc tu re items. The hig hest ran ge is achie vied when the an ten na is lo ca ted at the lowest point of the air craft fu se la ge. B. The in stal la ti on di men sions of the trans pon der an ten nas 1A032 is shown in Fig CAU TI ON : The trans pon der an ten na 1A032 is pro vi ded with a si li co ne rub ber gas ket which must also be in ter po sed bet ween the skin of the air craft and the an ten na. In air craft ha ving a woo den or plas tic airf ra me an elec tric coun terweight pla te or pa nel must be lo ca ted wit hin the fu se la ge at the anten na lo ca ti on with mi ni mum di men sions 40x40 cm (15.7x15.7 inch). C. An ten na ca ble RG-58C/U (0.9 db/m) or RG-223/U (0.6 db/m) can be used for the trans pon - der. If the ca ble length is lon ger than 2 m bet ween the unit and the an ten na, the ca ble type RG- 223/U is re com men ded. The ma xi mum cable length shouldn t be any more than 5 m. The com ple te loss of the an ten na ca ble mustn t be grea ter at than 3dB. Page 2-4

27 6. Pro gram ming of the Ad dress Mo du le INSTALLATION AND OPERATION The 24-bit ICAO ad dress once al lo ca ted by the lo cal authority is sto red for the as - sig ned trans pon der in the Ad dress Mo du le AM (01). The ad dress mo du le pro gram mer kit AMP (Ar ti cle-no ) is a tool for rea ding and sto ring fi xed air craft data into the Ad dress Mo du le (par al lel in - ter fa ce). This tool is for ser vi ce and main ten an ce only. The CD-ROM, which is part of the ad dress mo du le pro gram mer kit, in clu des a des - crip ti on of the pro gram ming pro ce du re. In sert the CD-ROM into a PC and fol low the in struc tions. If au to start is dis ab led on your PC, you have to start se tup.exe ma nu - al ly. 7. Avio nics data trans fer A. The is a data link trans pon der ac cor ding to RTCA DO-181C, re spec ti ve ly a le vel 2 trans pon der ac cor ding to Eu ro cae ED-73B.This stands for the ca pa bi li ty to trans fer data from the ground to a con nec ted ADLP or a si mi lar de vi ce and vice ver sa. B. The trans pon der trans mits in for ma ti on as re ply on a Ground In itia ted Comm-B (GICB) re quest or by me ans of the ex ten ded squit ter functi on. In both ca ses the va lid in for ma ti on must be avai la ble in the GICB re gis ters in the trans ponder. C. The trans pon der also trans mits in for ma ti on by me ans of the Air In itia ted Comm-B (AICB) functi on. In this case the in for ma ti on must be avai la ble in a spe ci al re gis ter in the trans pon der. The trans pon der an noun ces the mes sa ge and trans mits it af ter aut ho ri sa ti on from the ground sta ti on. D. In the ot her di rec ti on, the trans pon der is able to re cei ve in for ma ti on wit hin a Comm-A for mat from the ground sta ti on, which is then buf fe red and trans fer red to the con nec ted de vi ce. E. In the a sto ra ge de sign is im ple men ted for uplink- as well as for downlink mes sa ges. This me ans that all in for ma ti on that might be trans fer red from the trans pon der is buf fe red in si de the trans pon der first. F. The buf fers can be ac ces sed from an ADLP or a si mi lar de vi ce via the in ter face on the rear con nec tor J8. The in ter fa ce is mar ked with TISRX and TISTX in the air craft wi ring dia gram (see Fig. 2-4). G. The re la ted pro to col is spe ci fied in the at tach ment do cu ment Data Transfer Interface Protocol BXP 640X-XX-(XX). This manual is avai la ble at the Becker Product Support under the Article-No Page 2-5

28 7.1 Re mo te con trol A. As the is a re mo te con trol led trans pon der, it needs an additio nal con trol ling de vi ce. B. This may be the CU (XX), a spe ci al de sig ned con trol unit, which of fers the com ple te set of con trol functions and in di ca tions. C. The trans pon der may also be con trol led by anot her de vi ce (such as an FMS). D. Two in ter fa ces are avai la ble for that pur po se. E. One is on P9 at the rear of the trans pon der. It is mar ked with RX and TX in the con nec ti on dia grams. The trans pon der ac cepts and trans mits only con trol mes sa ges via this in ter fa ce. F. The ot her one is on J8. It is a com bi ned in ter fa ce which hand les con trol and data trans fer in par al lel. This in ter fa ce is mar ked with TISRX and TISTX in the air craft wi ring dia gram (see Fig.2-5). G. The pro to col for both in ter fa ces is des ri bed in the do cu ment BXP 6400 Ex tended Pro to col. This do cu ment is avai la ble at the Be cker Pro duct Sup port. 8. Set tings af ter in stal la tio n The fol lo wing des crip ti on is va lid for the re mo te trans pon der in connection with the con trol unit CU (XX). Also see tab le on the next page. Ins talla ti on mode is avai la ble from SBY mode only. To get into in stal la ti on mode press but ton SEL (G, see Fig. 3-1 in the ma nu al CU ), turn with ro ta ry en co - der (B) un til INS ap pe ars in the bot tom line of the dis play. Se lect by pres sing push-button (C). The in stal la ti on se tup is pro tec ted by pass word En ter pass - word and press sto re but ton (F). NOTE: If ins te ad of the CU (XX) anot her Con trol Unit is used, then the con trol pro - to col set tings must be car ried out as they are des cri bed in the document Control Interface Protocol. This manual is available at the Becker Product Support under the Article-No Page 2-6

29 Se lect with but ton (C) Se lect with ro ta ry en co der (B) Sto re but ton (F) ALTM SELECT GAR MIN / TRIMBLE NORTHSTAR UPS AT (BECKER BE6400) LORAN MA GEL LAN SHA DIN AR NAV GILHAM / PARALLEL default sto re sto re sto re sto re sto re store store store DIM MING IN PU T None (set il lu mi na ti on in ten si ty ma - nu al ly in the con fi gu ra ti on menu) de fault sto re +5V DC +14V DC +28V DC store sto re sto re SQUIT TER Short ACQ SQU * Default on off/on REPLY RATE LIMIT RPL RATE LMT re plies/sec. in Mode A/C (set ting in steps of 50) SPECIALS DATA LINK ** DE FAULT CON FIG *** ALT HIGH RESOL Er ror Latch LOW VOLT HIGH TEMP AN TEN NA RF PO WER DME ERR SQRT ERR CORE EE RE CEI VER FIX DATA AL TI ME TER DATA LINK Cle ar latch store store store sto re view only view only view only view only view only view only view only view only view only view only view only store * Trans pon ders equip ped for ex ten ded squit ter ope ra ti on should have a me ans to dis ab le ac qui si ti on squitters to facilitate the suppression of acquisition squitters when all TCAS units have been converted to receive extended squitter. ** Shall be dis ab led if no ADLP or si mi lar de vi ce is con nec ted. *** De fault con fig.: Dim ming in put none Bright ness 50% Al ti tu de dis play ed in ALT mode AI in SBY AI in ON II lu min. cha rac te ris tics max. ran ge Code 0000 VFR 0000 Flight num ber eight blanks Flight num ber not ac ti ve NOTE: If no type is avai la ble, this field in di ca tes not hing. Page February 2007

30 9. Chec king af ter installation A. Ge ne ral INSTALLATION AND OPERATION Af ter the in stal la ti on, check the re mo te con trol led trans pon der in con juncti on with the con trol unit to en su re sa tis fac to ry ope ra ti on of the trans pon der. B. Pre-flight check using self test Switch-on test: Switch the trans pon der ope ra ting mode switch from OFF to SBY. A po wer-on built-in test (PBIT) then fol lows au to ma ti cal ly for 1 se cond. Du ring the test WAIT is in di ca ted. If the test was suc cess ful, the unit swit ches then to the mode set on the mode switch. Test trig ge red (IBIT): Press the SEL but ton and STO but ton at the same time in mode ON or ALT. A test of all avai la ble test rou ti nes then fol lows for 1 se cond. Du ring the test, IBIT is in di ca ted on the dis play. If the IBIT was suc cess ful, the trans pon der swit ches im me di ate ly into the nor mal ope ra ting mode. In case of a fault ap pe ars the re port FAI LU RE in the dis play. Switch OFF the trans pon der at the fault in di ca ti on. C. Check of the ad dress mo du le The installation company has to make sure that the corresponding address module AM is in stal led with the transponder and that the address module is pro gram med correctly. It is recommended to connect the address module with the aircraft tightly. D. Test and ad just ment of trans mit fre quen cy Set code 0000 on the trans pon der and mode A in ter ro ga ti on on the ramp test set. Check trans mit fre quen cy by me ans of the ramp test set. Trans mit frequen cy must be 1090 ± 1 MHz. If out of ran ge send the trans pon der to aut ho rised ser vi ce. E. Check of the trans mit po wer Af ter in stal la ti on of equip ment and an ten na the trans mit po wer has to be che - cked at the an ten na end of the fee der line: Re qui re ment: 125 W (21 dbw) at class 1 trans pon der 70 W (18.5 dbw) at class 2 trans pon der WAR NING: Ra di ati on risk: A safe dis tan ce to the in stal led an ten na must be en su red by cor re spon ding in stal la ti on mea su res around hu man body da ma ge (e.g. at the eyes) and / or avoid the in flam ma ti on of com bus ti ble ma te ri als by ra di ated ener gy. Page 2-8

31 Fig. 2-1 In stal la ti on di men sions, me as ures in mm Page 2-9

32 Fig. 2-2 Moun ting in stal la ti on di men sions, mea su res in mm Page 2-10

33 Fig. 2-3 In stal la ti on di men sions 1A032 Page 2-11

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