Becker BXP6403 Manuale utente

NSCM: D2356

Control Unit

CU 6401-1-(XX)

(for Mode S transponder BXP 6402-XR)

INSTALLATION AND OPERATION

Ma nu al DV 69803.03 PN 0584.096-071

Be cker Flug funk werk GmbH • Ba den-Airpark B 108 • 77836 Rhein müns ter • Ger ma ny

Te le pho ne +49 (0) 7229 / 305-0 • Fax +49 (0) 7229 / 305-217

http://www.be cker-avionics.de · e-mail: info@be cker-avionics.de or sup port@be cker-avionics.de

Initial Issue:

December 2005 34-50-10 February 2007

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 2007 02/07 Becker

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34-50-10

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CU 6401-1-(XX)

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34-50-10 December 2005

LIST OF EF FEC TI VE PA GES

SUB JECT PAGE DATE SUB JECT PAGE DATE

Tit le Page TP-1 Feb. 2007

TP-2 2005

Record of Revisions ROR-1 Feb. 2007

ROR-2 blank

List of Effective Pages LEP-1 Feb. 2007

LEP-2 blank

Introduction Intro-1 Dec. 2005

Intro-2 Dec. 2005

Intro-3 Dec. 2005

Intro-4 blank

Table of Contents I-I Feb. 2007

I-II blank

General Description 1-1 Feb. 2007

1-2 Feb. 2007

1-3 Feb. 2007

1-4 Feb. 2007

Table of Contents II-I Dec. 2005

II-II blank

Installation 2-1 Feb. 2007

2-2 Dec. 2005

2-3 Feb. 2007

2-4 Dec. 2005

2-5 Dec. 2005

2-6 Dec. 2005

Table of Contents III-I Dec. 2005

III-II Dec. 2005

Operation 3-1 Dec. 2005

3-2 Dec. 2005

3-3 Dec. 2005

3-4 Dec. 2005

3-5 Dec. 2005

3-6 Dec. 2005

3-7 Dec. 2005

3-8 Dec. 2005

3-9 Dec. 2005

3-10 Dec. 2005

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34-50-10 December 2005

IN TRO DUC TI ON

1. Gen eral

The Con trol Unit CU 6401-1-(XX) for the re mo te con trol led Mode S trans pon der

BXP 6402-XR-(XX) is des cri bed in this ma nu al “Installation and Operation”.

2. Manufacturer

The Con trol Unit was de ve lo ped and is ma nu fac tur ed by :

Be cker Flug funk werk GmbH

Ba den-Airpark B 108

77836 Rhein müns ter / Germany

Te le pho ne: +49 (0) 7229 / 305-0

Te le fax: +49 (0) 7229 / 305-217

http://www.be cker-avionics.de

e-mail: 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. 12 100 20985

LI CEN SES AND AP PRO VALS

DE.21G.0075 Ap pro val as ma nu fac tu rer to EASA PART 21

DE.145.0166 Ap pro val as main ten an ce or gani za ti on to

EASA PART 145

3. Sa fe ty information

n

The installation of the transponder control unit into an aircraft may be car-

ried out only by an authorized installation company. The country regulations

always have to be observed.

n Do not con nect the unit to AC sour ces.

n

Make sure that the unit is con nec ted to a DC sour ce ≤ 33 V DC.

n

The unit should be pro tec ted from the air craft po wer supp ly by a de di ca ted

1 A cir cuit brea ker.

n

Do not con nect the unit with re ver sed po la ri ty to the DC sour ce.

n

Do not switch on the unit be fo re the air craft en gi nes are started. Switch off

the unit be fo re the en gi nes are shut down.

INSTALLATION AND OPE RA TI ON

CU 6401-1-(XX)

IN TRO Page 1

34-50-10 December 2005

n

Do not operate the unit under ambient temperatures below -20° C and

above + 70° C.

n

The programming of the transponder address module AM 6400-1 with the

ICAO 24-bit address of the aircraft must be carried out only at an installa-

tion company or in the manfacturer factory.

4. Lay out of manual

The ma nu al is divi ded into three chapters:

- GE NE RAL DES CRIP TI ON

- IN STAL LA TI ON

- OPE RA 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 Air craft Ad dress (24-bit ICAO)

ADLP Avio nics Data Link Processor

AI Air craft Iden ti fier (tail num ber)

ALT Al ti tu de or trans pon der ALT mode

ATC Air Traf fic Con trol

BIT Built-In Test

CBIT Con ti nu ous Built-In Test

CCS Com pa ny Call Sign

CU Con trol Unit

CS Call Sign

DV Manual identification number

EASA Eu ro pe an Avia ti on Sa fe ty Agen cy

ELS Ele men ta ry Sur veil lan ce

EHS En han ced Sur veil lan ce

es e = Extended squit ter and s = SI capability

FAA Fe de ral Avia ti on Ad mi nis tra ti on

FL Flight Le vel

FN Flight Num ber

GND Ground

ICAO In ter na tio nal Ci vil Avia ti on Or gani za ti on

IBIT In itia ted Built-In Test

ID Iden ti fier

IDT Ident (Iden ti fi ca ti on)

NSCM Nato Supp ly Code of Manufacturers

ON Trans pon der ON mode (wit hout al ti tu de trans mis si on)

PBIT Po wer-on Built-In Test

PN Part Number

R Reply

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34-50-10 December 2005

RX Recei ver

SBY Stand by mode

SEL Se lec ti on

SI Sur veil lan ce Iden ti fier

STO Sto re

SUPP Supply voltage DC

TX Transmitter

VFR Vi su al Flight Ru les

XPDR Transponder

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34-50-10 December 2005

TAB LE OF CON TENTS

GE NE RAL DES CRIP TI ON Page

1. Ap pli ca ti on 1-1

2. Ge ne ral des crip ti on 1-1

3. Tech ni cal data 1-2

A. General data 1-2

B. Environmental qualification 1-3

4. Soft wa re 1-4

5. Sys tem ap pro vals 1-4

6. Equipment 1-4

7. Ac ces so ries 1-4

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GE NE RAL DES CRIP TI ON

1. Ap pli ca ti on

To get her with the Mode S re mo te trans pon der BXP 6402-XR-(XX) the Con trol Unit

CU 6401-1-(XX) forms the air craft part of the air traf fic con trol sys tem.

2. Ge ne ral des crip ti on

A. The CU 6401-1-(XX) con trol unit is de sig ned for in stal la ti on in the in stru ment

pa nel of air craft. The di men sions corre spond to the stan dard in stru ment size

with a 58 mm (2¼ inch) dia me ter.

B. All con trols are lo ca ted on the front pa nel of the unit. The 15-pole unit con nec

-

tor is lo ca ted at the rear side of the con trol unit.

C. A se ri al in ter fa ce RS-422 for con nec ti on of the re mo te con trolled trans pon der

BXP 6402-XR-(XX) is avai la ble at the unit con nec tor.

D. The CU 6401-1-(XX) con trol unit in con juncti on with the BXP 6402-XR-(XX) re -

mo te trans pon der provides the fol lo wing features:

(1) In the se lec ti ve mode (Mode S), the con trol ler on the ground can in ter-

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) Re gis ter ca pa bi li ty for ele men ta ry sur veil lan ce (ELS) and en han ced sur-

veil lan ce (EHS)

(4) Ex ten ded squit ters trans mis si on

(5) Data link ca pa bi li ty

E. In he rent fea tu res:

(1) Mode A - in this mode, the 4096 cha rac ter code set on the con trol head

is sent as a re ply to in ter ro ga ti on from a ground sta ti on.

(2) Mode C - in this mode, the en co ded al ti tu de is sent in ad di ti on to the

mode A re ply. The al ti tu de in for ma ti on must be de li ver ed from an ex ter-

nal de vi ce.

(3) A spe ci al iden ti fier pul se (SPI) can be ac ti vat ed by pres sing the IDT

but ton in Mode A/C and Mode S.

(4) Selftests (BITs). The Initiated Built-In Test (IBIT), the Continuous Built-In

Test (CBIT) and the Power-on Built-In Test (PBIT) are integrated in the

transponder.

INSTALLATION AND OPERATION

CU 6401-1-(XX)

Page 1-1

34-50-10

February 2007

3. Tech ni cal data

A. General data

Supply voltage 10.0 to 33.0 V DC

Typical con sump ti on 0.045 A at 14 V (il lum. off)

0.034 A at 28 V (il lum. off)

0.138 A at 14 V (il lum. max.)

0.080 A at 28 V (il lum. max.)

Panel il lu mi na ti on con trol input

Illumination con trol current max. 1 mA at 28 V

Illumination co lor (dis play and bu ttons) white

Control in ter fa ce RS-422

Power-up time 2 s (in clu ding in ter nal self-test)

Internal fuse pro tec ti on F 1 A

External fuse pro tec ti on 1 A

Operating al ti tu de 50000 ft. max.

Ope ra ting tem pe ra tu re ran ge - 20° C to + 55° C

(short-time + 70° C)

Storage tem pe ra tu re ran ge - 55° C to + 85° C

Environmental con di tions in ac cor dan ce with

EU RO CAE/RTCA

ED-14D/DO-160D

Mechanical di men sions:

- Front pa nel 61.3 x 61.3 (H x W)

(2.413 x 2.413 inch)

- In stru ment size dia me ter 58 mm (2¼ inch)

- Case depth 65 mm (2.559 inch)

Weight 0.22 kg (0.485 lb)

INSTALLATION AND OPERATION

CU 6401-1-(XX)

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February 2007

B. Environmental qualification

EUROCAE/RTCA ED-14D/DO-160D

Condition 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 4.5.1 D1 -55 deg C

Low Ope ra ting Tem pe ra tu re 4.5.1 D1 -20 deg C,

High Ground Sur vi val Temp 4.5.2 D1 +85 deg C

High Short-Time Ope ra ting Temp. 4.5.2 D1 +70 deg C

High Ope ra ting Temp. 4.5.2 D1 +55 deg C

In-flight Loss of Coo ling 4.5.4 Z No for ced coo ling re qui red – No test

re qui red

Al ti tu de 4.6.1 D1 50000 ft

De com pres si on 4.6.2 Not applicable

Over pres su re 4.6.3 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 bi -

li ty

18.0 B Equip ment tes ted to Ca te go ry B

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 -

cep ti bi li ty

22.0 A3E3X Equip ment tes ted to Ca te go ry A3E3X

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

INSTALLATION AND OPERATION

CU 6401-1-(XX)

Page 1-3

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February 2007

4. Soft wa re

The con trol unit CU 6401-1-(XX) is con trol led by a mi cro con trol ler in the con trol

head. 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.210.322 ETSO-2C112a

FAA TSO-C112

6. Equipment

CU 6401-1-(01) Control Unit Article-No. 0572.896-915

7. Ac ces so ries

CK5000-C Con nec tor kit (crimp) Article-No. 0511.781-954

1 D-Sub jack, 15-pin

CK5000-S Con nec tor kit (soldering) Article-No. 0511.791-954

1 D-Sub jack, 15-pin

Ma nu als:

In stall ati on and Operation CU 6401-1-(XX) Article-No. 0584.096-071

Main te na nce and Repair CU 6401-1-(XX) Article-No. 0584.101-071

Control Interface Protocol BXP 6402-XR-(XX) Article-No. 0590.241-071

INSTALLATION AND OPERATION

CU 6401-1-(XX)

Page 1-4

34-50-10 February 2007

TAB LE OF CON TENTS

IN STAL LA TI ON Page

1. Ge ne ral 2-1

2. In spec ti on be fo re in stal la ti on 2-1

3. Me cha ni cal in stal la ti on 2-1

4. Air craft wi ring 2-1

5. Set tings af ter in stal la ti on 2-2

6. Chec king af ter in stal la ti on 2-4

Fig. 2-1 In stal la ti on di men sions CU 6401-1-(XX) 2-5

Fig. 2-2 Pro po sal for air craft wi ring CU 6401-1-(XX) 2-6

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IN STAL LA TI ON

1. Ge ne ral

In stal la ti on of the con trol unit CU 6401-1-(XX) 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 o n

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 con trol unit 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 out for the following defects:

(1) Dirt, dents, scratches, corrosion, broken fastening elements on housing and

housing parts.

(2) Dirt and scratches on nameplate, front plate and inscriptions.

(3) Dirt, bent or broken pins and cracked insert of unit connector.

(4) Dirt, stiffness and mechanical damage to the pushbuttons, rotary switches

and LC displays.

(5) Missing screws.

3. Me cha ni cal in stal la ti on

The con trol unit is de sig ned for in stal la ti on in the in stru ment pa nel of an aircraft. It

is con struc ted for moun ting be hind the pa nel. The cir cu lar cut out and the moun ting

ho les are to be dril led in ac cor dan ce with the small in stru ment size. 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 are gi ven in Fig. 2-1. At tach ment is by me ans of four

screws M3x12, which are in clu ded in the de li very.

4. Air craft wi ring

A. The air craft wi ring of the con trol unit is shown in Fig. 2-2.

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 con trol unit in ter wi ring.

IN STAL LA TI ON AND OPE RA TI ON

CU 6401-1-(XX)

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B. Pin con nec tions of the unit con nec tor P1

The unit con nec tor type is D-SUB 15-pole male.

Pin Pin Name Pin Des crip ti on Sour ce Des ti na ti on Re com men -

ded cable

type

1

2

TX+

TX-

RS-422 data interface CU 6401-1-(XX) BXP 6402-XR-(XX) 2xAWG26,

shiel ded

and twisted

3 GND DC supp ly Ground,

addi tio nal con nec ted

to Pin 9 and 10

DC supp ly vol ta ge

Ground

CU 6401-1-(XX) AWG20

4

5

RX+

RX-

RS-422 data in ter face BXP 6402-XR-(XX) CU 6401-1-(XX) 2xAWG26,

shiel ded

and twisted

6 ILL A Il lu mi na ti on control Il lum. vol ta ge Il lum. in put AWG26

7 Not connected

8 ILL B Il lu mi na ti on GND Il lum. ground Il lum. in put AWG 20

9

10

GND Ground, ad di tio nally

con nec ted to Pin 3

DC supp ly vol ta ge

Ground

CU 6401-1-(XX) 2xAWG20

11

12

SUPP Supp ly vol ta ge in put,

ex ter nal 1 A fuse for

cur rent pro tec ti on

DC supp ly vol ta ge

sour ce 10 to 33 V

CU 6401-1-(XX) 2xAWG20

13 ON ON/OFF sig nal CU 6401-1-(XX) BXP 6402-XR-(XX) AWG26

14 Not con nected

15 Ext. ID Ex ter nal Ident Ident but ton ext. CU 6401-1-(XX) AWG 26

C. Il lu mi na ti on

Con nect the il lu mi na ti on vol ta ge to pin 6 of P 1 and at tach pin 8 to the il lu-

mi na ti on ground. Set il lu mi na ti on inten si ty ma nu al ly in the con fi gu ra ti on me-

nu.

5. Set tings af ter in stal la ti on

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), 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 “6435”. En ter pass word and press sto re but ton (F).

See tab le on the next page.

INSTALLATION AND OPE RA TI ON

CU 6401-1-(XX)

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