6 DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

ATA SYSTEM : 25

TITLE : EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIR

UPPER COCKPIT DOOR PLATE COVER

MODIFICATION No. : 51911D44499

This page transmits Revision No. 01 of Service Bulletin No. A340-

ADDITIONAL WORK

No additional work is required by this revision for aircraft m

previous issue.

REASON

This revision has been issued to add the removal/installation 

Hijack Camera, update the effectivity, add some covers to the 

re-identified and make some other minor changes.

CHANGES

SUMMARY :

— Para. EFFECTIVITY - updated.

— Para. MANPOWER - Manhouers updated.

PLANING INFORMATION

— Para. A.(2)(b), Operator AIB added. Operator BOE and BUB de

— Para. A.(3), Spares updated.

— Para. F., Approval sentence has been changed.

— Para. G, Manhouers updated.

— Para. J., Subsequent references added:

. Elec. Std. Practices Manual 20-25-51 20-33-44 20-52-21 20

. Standards Manual.

. Consumable Material List.

— Para. K., Publications affected added:
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

— Para. E., Parts to be re-identified by the operator updated

ACCOMPLISHMENT INSTRUCTION

— Para. A.(1)(b), In case of contamination refer to ESPM 20-5

— Para. A.(1)(k), Removal of Anti Hijack Camera added.

— Para. A.(2)(b), Identification of access Panel added.

— Para. A.(2)(g), Cable tie installation and tooling.

— Para. A.(2)(h), Continuity Test.

— Para. D.(4), Installation of Anti Hijack Camera added.

ILLUSTRATIONS

— Figure 1, Sheet 2 amended

— Figure 1, Sheet 4 amended

— Figure 1, Sheet 5 amended

— Figure 5, Sheet 2 amended

— Figure 5, Sheet 7 amended

NOTE : Layout changes due to computerization of this revision 

identified.

FILING INSTRUCTIONS

This Service Bulletin has been generated electronically and is 

complete document. Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service B

HISTORY OF PREVIOUS REVISIONS

No previous revisions.

REVISION SEQUENCE

ORIGINAL : Oct 12/04

REVISION No. : 01 — Apr 25/05

2
6 DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This summary is for information only

and is not approved for modification of the aircraf

ATA SYSTEM : 25

TITLE : EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIR

UPPER COCKPIT DOOR PLATE COVER

MODIFICATION No. : 51911D44499

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During the accomplishment of SB A340-25-4181 (Installation of the 

Penetration Resistant Cockpit Door) it was found that the electri

7450VB, installed on the cover of the upper cockpit door frame, i

from the cabin side. Therefore, the protection of this harness mu

This Service Bulletin introduces :

— the re-routing of the electrical harness 7450VB,

— the installation of a protection plate for the electrical harne

This Service Bulletin has been validated on A340-600 aircraft MSN 

Accomplishment of this Service Bulletin improves cockpit security 

access to the electrical harness from the cabin side.

EFFECTIVITY

This Service Bulletin is applicable to these operator(s) :

EVALUATION TABLE

COMPLIANCE RECOMMENDED CANCELS INSPECTION SB 

POTENTIAL AD NO A/C OPERATION AFFECTED 

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED 

COST SAVING NO ETOPS AFFECTED 

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED 

KIT PRICE (USD)

254217D02R00

190
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

REFERENCES/REPERCUSSIONS

TFU : None

OEB : None

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHERS : None

NATURE OF THE WORK

Kit 254217D02R00

AIRCRAFT : YES

EQUIPMENT : NO

HARD : NO

SOFT : NO

OBRM : NO

MANPOWER

Kit 254217D02R00

MATERIAL INFORMATION

AIRCRAFT DATA

Protection plate, screws, washers, nuts, clamps, ties, insert

APPENDICES

None

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

2
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

3
6 DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

ATA SYSTEM : 25

TITLE : EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIR

UPPER COCKPIT DOOR PLATE COVER

MODIFICATION No. : 51911D44499

This document contains AIRBUS PROPRIETARY INFORMATION and shall a

remain the property of AIRBUS; no intellectual property right or 

granted by AIRBUS in connection with any information contained in 

delivered on the express condition that the said document and the 

contained in it shall be treated as confidential, shall not be us

purpose other than that for which it is hereby delivered. It shal

disclosed in whole or in part to third parties and shall not be d

any manner (except for the purposes of performing the tasks descr

and provided that any recipient of such document shall comply wit

conditions herein), without AIRBUS prior written consent.

1. PLANNING INFORMATION

A. EFFECTIVITY

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft 

0002-0009 0011 0013-0016 0018-0029 0031-0035 00

0043-0044 0046-0049 0051-0053 0056-0058 0061 00

0078-0081 0084-0085 0088-0091 0093-0094 0097 010

0114-0115 0117 0123 0125-0126 0128-0129 0131 01

0141-0142 0145-0147 0149-0152 0154 0156-0161 01

0166-0170 0173-0176 0178-0180 0182 0185-0187 019

0196-0197 0199 0201-0202 0207-0208 0210 0212-02

0225 0227-0228 0233 0235-0237 0239 0242-0243 024

0257 0260 0263-0264 0268 0270 0273-0274 0278 02

0292 0297 0302 0304 0307 0310 0318-0319 0321 03

0331-0332 0335 0347 0352 0354-0355 0359 0363 03

0377-0379 0381 0385 0387 0390 0395 0399 0402 040

0413-0415 0424 0429-0430 0433-0435 0438 0442 044

0459 0467 0470 0474 0483 0528 0538 0541 0544-054

0559 0561-0562 0582 0585 0590
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

OPERATOR MSN

39Z 0151

50Z 0009

ACA 0088 0150 0154 0167 0170 0175 0179 0

AFR 0005 0007 0029 0049 0078 0084 0168 0

0210 0237 0245 0246 0260 0289 0307 0

0377 0399

AIB 0031

AJM 0048 0216 0257

ALK 0032 0033 0034 0367 0374

ARG 0063 0074 0080 0085

AUA 0075 0081 0169 0263

B3R 0046

BWA 0016 0093

CAL 0402 0406 0411 0415 0433 0528 0541

CES 0129 0131 0141 0161 0182

CPA 0123 0126 0128 0136 0137 0142 0147 0

0218 0220 0227 0228 0381

CRX 0538 0545 0546 0556 0559 0561 0562 0

CXN 0192 0199 0201 0242 0243 0264

DLH 0020 0024 0027 0028 0035 0047 0051 0

0135 0158 0213 0233 0252 0274 0297 0

0327 0335 0347 0352 0354 0355 0379 0

ETD 0117

GFA 0039 0040 0097 0103 0133 0212 0215 0

IBE 0125 0134 0145 0146 0193 0197 0217 0

0329 0332 0378 0387 0414 0459 0474 0

KAC 0089 0090 0101 0104

LAN 0359 0363 0429 0442

M3R 0061

MAU 0076 0094 0152 0194 0268

MSR 0156 0159 0178

OAL 0235 0239 0280 0292

PAL 0173 0176 0187 0196

2
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(c) Effectivity by MSN and Kit/Configuration

The kits and configurations applicable to these 

at the end of this list:

0002-0009 0011 0013-0016 0018-0029 0031-0035 00

0043-0044 0046-0049 0051-0053 0056-0058 0061 00

0078-0081 0084-0085 0088-0091 0093-0094 0097 010

0114-0115 0117 0123 0125-0126 0128-0129 0131 01

0141-0142 0145-0147 0149-0152 0154 0156-0161 01

0166-0170 0173-0176 0178-0180 0182 0185-0187 019

0196-0197 0199 0201-0202 0207-0208 0210 0212-02

0225 0227-0228 0233 0235-0237 0239 0242-0243 024

0257 0260 0263-0264 0268 0270 0273-0274 0278 02

0292 0297 0302 0304 0307 0310 0318-0319 0321 03

0331-0332 0335 0347 0352 0354-0355 0359 0363 03

0377-0379 0381 0385 0387 0390 0395 0399 0402 040

0413-0415 0424 0429-0430 0433-0435 0438 0442 044

0459 0467 0470 0474 0483 0528 0538 0541 0544-054

0559 0561-0562 0582 0585 0590

SAS 0413 0424 0430 0435 0450 0467 0470

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446

THY 0023 0025 0057 0115 0180 0270 0331

UAE 0139 0149 0163 0166 0185 0190 0202 0

VIR 0002 0003 0013 0015 0058 0114 0164 0

KIT No. QTY PER A/C CONFIGURATION

254217D02R00 1 No

3
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Cover F2527487101200

Cover F2527487101400

Cover F2527487101600

Cover F2527487101800

Cover F2527487102000

Cover F2527487102200

Cover F2527487102400

Cover F2527487102600

Cover F2527487102800

Cover F2527487103000

Cover F2527487103200

Cover F2527487103400

Cover F2527487103600

Cover F2527487103800

Cover F2527487104000

Cover F2527487104200

Cover F2527487104400

Cover F2527487104600

Cover F2527487104800

Cover F2527487105000

Cover F2527487105200

Cover F2527487105400

Cover F2527487105600

Cover F2527487105800

Cover F2527487106000

Cover F2527487106200

Cover F2527487106400

Cover F2527487106600

Cover F2527487106800

Cover F2527487600200

Cover F2527487601600

Cover F2527487601800

Cover F2527487604200

Cover F2527487604800

Cover F2527487605600

Cover F2527487606000

Cover F2527487606600

Cover F2527487606800

B. CONCURRENT REQUIREMENTS

Service Bulletin(s) to be accomplished previously or simu

Service Bulletin No. A340-25-4181 Mod. No. 50014D44099

4
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

the protection of this harness must be improved.

(2) Objective/Action

This Service Bulletin introduces :

— a re-routing of the electrical harness 7450VB,

— the installation of a protection plate for the elec

7450VB.

This Service Bulletin has been validated on A340-600 

0436.

(3) Advantages

Accomplishment of this Service Bulletin improves coc

by denying access to the electrical harness from the 

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Kit 254217D02R00

(a) Get access to the electrical harness 7450VB of t

door release system.

(b) Modify the cover of the upper cockpit door frame

(c) Install the cable harness 7450VB to the cover of 

cockpit door frame and the RH cockpit door post

E. COMPLIANCE

(1) Classification

Recommended

(2) Accomplishment Timescale

In accordance with operators' maintenance schedule.

5
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are 

direct labor cost to do the work. These estimates assume 

will be done by experienced personnel, and may need to be 

upwards to suit operators' circumstances. The estimates do 

the time to prepare, plan or inspect the work. Manufactur

procurement of parts and tools, drying time for paints, s

and general administration work are also not included.

Kit 254217D02R00

H. WEIGHT AND BALANCE

Kit 254217D02R00

Manufacturers Empty Weight : 0.402 kg (0.89 lb)

Effect on Balance : 4.133 kgm (29.89 lb.ft)

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Get Access 

Modification 

Test 

Close-up 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Aircraft Maintenance Manual (AMM) : 06-41-53 12-34-24 

23-72-51 25-13-44 

52-10-00 52-51-00

Standards Manual (SM)

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) : 20-25-51 20-33-00 

20-52-21 20-55-00

6
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

L. INTERCHANGEABILITY/MIXABILITY

None

Aircraft Maintenance Manual (AMM) : 52-51-00 52-51-11 

Aircraft Schematic Manual (ASM) : 52-51-00

7
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This Page Intentionally Left Blank

8
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

of this Service Bulletin. The address is :

AIRBUS

MATERIEL SUPPORT CENTER

PO BOX 630262

22312 HAMBURG

GERMANY

(2) Price and Availability

Kit 254217D02R00

Cost : 190 US Dollars

Availability : 90 calendar days from receipt of orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

so that we can try to comply with your requirements.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishme

Service Bulletin.

C. LIST OF COMPONENTS

Kit 254217D02R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

3 NAS1833C08-370 4 EA INSERT

4 MS21250-03012 1 EA BOLT

5 NAS1149CN949R 1 EA WASHER

6 DAN125-4 4 EA WASHER

7 NAS1102-08-6 4 EA SCREW

8 F2527496220200 1 EA WIREPROT

9 NAS1096-3-14 2 EA SCREW

10 ASNA0113-56ADL 2 EA WASHER

11 MS21919WCH7 4 EA CLAMP

12 NAS1096-2-10 4 EA SCREW

13 MS21042L08 4 EA NUT

9
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

() 

(2) Components

None

E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR

DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C 

Vaseline 04-012 As required

Coating 07-001 As required

Adhesive 08-010A As required

Cleaning Agent 11-026 As required

Cloth, lint-free 19-003 As required

ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT

1 F2528716800200 COVER F2527487100000 03

1 F2528716800600 COVER F2527487100400 03

1 F2528716801000 COVER F2527487100800 03

1 F2528716801400 COVER F2527487101200 03

1 F2528716801600 COVER F2527487101400 03

1 F2528716801800 COVER F2527487101600 03

1 F2528716802000 COVER F2527487101800 03

1 F2528716802200 COVER F2527487102000 03

1 F2528716803200 COVER F2527487103000 03

1 F2528716803600 COVER F2527487103400 03

1 F2528716804000 COVER F2527487103800 03

1 F2528716804200 COVER F2527487104000 03

1 F2528716804400 COVER F2527487104200 03

1 F2528716805000 COVER F2527487104800 03

1 F2528716805600 COVER F2527487105400 03

1 F2528717000200 COVER F2527487600200 03

1 F2528717001600 COVER F2527487601600 03

1 F2528717001800 COVER F2527487601800 03

1 F2528717004200 COVER F2527487604200 03

1 F2528717004800 COVER F2527487604800 03

1 F2528717005600 COVER F2527487605600 03

1 F2528717006000 COVER F2527487606000 03

10
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

F. TOOLING — PRICE AND AVAILABILITY

None

G. SPECIAL TOOLS

None

11
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This Page Intentionally Left Blank

12
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(1) Preparation

(a) Electrically ground the aircraft (Refer to AMM 

block 201).

(b) In case of contermination refer to ESPM 20-55-00

(c) Put suitable access platforms in position.

(d) In the cockpit, on the panel 235VU, make sure t

push-button switches are released :

— BAT 1, BAT 2, APU BAT,

— GEN 1, 2, 3, 4 APU GEN,

— EXT A B.

(e) Open, safety and tag this these circuit breaker

(f) Make sure that there are warning notices in the 

tell persons not to operate the push-button swit

overhead panel :

— 211 VU (EMER ELEC PWR)

— 235 VU (ELEC).

(g) Make sure that there are warning notices in the 

tell persons not to start the APU.

(h) Make sure that the external connectors are not 

the aircraft receptacles EXT PWR A (B).

(i) Make sure that a warning notice is on the access 

tell persons not to connect the external power 

(j) Open the passenger/crew door 831 (Refer to AMM 

block 201).

(k) In the cockpit, remove the Camera Anti Hijack Sy

AMM 23-72-51 Page block 401.

PANEL DESIGNATION FIN LOCA

722VU CKPT DOOR LATCH 1MQ 39 V

13
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

plates necessary to get access to the modificat

equipment and wiring.

(2) Standard Practices

(a) Refer to the AIRBUS Standards Manual (SM) if yo

numbers for the hardware components in the relat

which you can not identify in the LIST OF COMPON

Service Bulletin. The SM will give you the corre

to part number relationship.

(b) For identification of access Panel, refer to AMM 

block 001.

(c) For the specification of the material numbers (M

refer the to Consumable Material List(CML).

(d) Do the electrical bonding (Refer to AMM 20-28-00 

201) with Pure Mineral Vaseline (Mat No. 04-012) 

Electrical Bonding Coating (Mat No. 07-001) .

(e) It is recommended to tag the retained parts and 

location to make the installation easier.

(f) Obey the instructions of the wiring installatio

ESPM 20-33-00).

(g) For cable tieinstallation and torling, refer to 

20-33-44 and ESPM 20-25-51.

(h) Do a continuiy test of new and of modified wire

ESPM 20-52-21.

(i) To install new wires, cut them to the necessary 

the terminals and connect them.

B. MODIFICATION

(1) Kit 254217D02R00

Refer to Figure 1

Refer to Figure 2

Refer to Figure 3

Refer to Figure 4

Refer to Figure 5

Refer to Figure 6

Refer to Figure 7

14
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

1 From the secure part, item (28) of the RH coc

post, as shown on Figure 1 , Sheet 4 , Detai

and

2 Disconnect the plug 25MQ-A from the key pad 2

3 From the plug 25MQ-A remove, as shown on Figu

, Detail F :

4 Remove the wires of the cable harness 7450VB

from the plug 25MQ-A.

5 From the RH cockpit door post remove, as show

, Sheet 2 , Detail C and Sheet 3 , Detail D 

and

6 Remove as shown on Figure 1 , Sheet 4 , Deta

and, as shown on Figure 1 , Sheet 4 , Detail 

1 cover Item (2

2 screws Item (2

1 cable tie Item (2

1 plug cover Item (2

2 screws with

clamps

Item (2

1 secure part Item (2

1 cover plate Item (2

6 screws Item (3

5 spacers Item (3

10 screws Item (3

9 screws Item (3

9 washers Item (3

3 clamps Item (3

6 clamps Item (3

9 spacers Item (3

15
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 , Sheet 5 , Detail L and to the Wir

Figure 7 .

9 From the cover, item (1) remove, as shown on 

Sheet 2 , Detail C :

and disconnect the wires of the electrical ha

from the limit switch.

10 From the cover, item (1) remove, as shown on 

Sheet 5 , Detail K :

11 Remove the electrical harness 7450VB, item (2

cover of the cockpit door frame, item (1).

(b) Modify the cover of the cockpit door frame.

Refer to Figure 2

Refer to Figure 3

Refer to Figure 4

1 From the cockpit door posts remove as shown o

Sheet 2 :

and

2 Remove from the cover, item (1), as shown on 

Sheet 1 :

cable ties Item (4

2 screws Item (3

1 limit switch Item (3

1 cover Item (1

1 screw Item (4

2 screws Item (4

1 washer Item (4

2 washers Item (4

3 covers Item (4

4 cable mounts Item (4

16
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

5 Drill four holes to a diameter of 14.5 mm (0.

upper edge of the cover, item (1), as shown o

Sheet 2 , Detail C and Section A-A.

6 In the upper edge of the cover, item (1), in

adhesive (Mat No. 08-010A) as shown on Figu

, Detail C and Section A-A :

7 Re-identify the cover, item (1), as given in 

2.E., PARTS TO BE RE-IDENTIFIED BY THE OPERAT

8 To the cockpit door posts install, as shown o

Sheet 2 , Detail C :

with

and

(c) Install the cable harness 7450VB to the cover of 

door frame and the RH cockpit door post.

Refer to Figure 5

Refer to Figure 6

Refer to Figure 7

1 Feed the electrical cable harness 7450VB, ite

the cover, item (1), as shown on Figure 5 , S

Detail C and Sheet 7 , Detail L.

2 Connect the electrical harness 7450VB, item 

release latches 30MQ, 31MQ and 32MQ, as shown 

Sheet 2 , Detail C and Sheet 3 , Detail E and 

to the Wiring Diagram, Figure 6 .

4 inserts NAS1833C08-370 Item 3

1 cover F25287168XXX00 Item (1

2 screws NAS1096-3-14 Item 9

1 screw MS21250-03012 Item 4

2 washer ASNA0113-56ADL Item 10

1 washers NAS1149CN949R Item 5

3 covers Item (4

17
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

5 To the cover, item (1) install, as shown on 

Sheet 7 , Detail L :

and

6 Attach the additional wire length in a loop t

electrical harness as shown on Refer to Figu

:

7 To the RH cockpit door post install, as shown 

Sheet 2 , Detail C and Sheet 3 , Detail E and 

with

8 To the RH cockpit door post install, as shown 

Sheet 2 , Detail C and Sheet 3 , Detail D :

9 Install as shown on Figure 5 , Sheet 5 , Deta

with

NOTE (01) Before you install the secure part

and the cover plate (29) feed the w

key pad plug 25MQ-A through the hol

1 limit switch Item (3

2 screws Item (3

2 ties NAS933401-03 Item 15

6 clamps Item (3

3 clamps Item (3

9 spacer Item (3

9 screws Item (3

9 washers Item (3

5 spacer Item (3

10 screws Item (3

1 secure part Item (2

1 cover plate Item (2

6 screws Item (3

18
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

11 To the plug 25MQ-A install, as shown on Figu

, Detail K :

12 Connect the plug 25MQ-A to the key pad 25MQ.

13 To the secure part, item (28) of the RH cock

install, as shown on Figure 5 , Sheet 6 , Det

and

14 To the cover, item (1) install as shown on 

Sheet 7 , Detail L and N :

with

C. TEST

(1) Remove the safety clips and tags and close these cir

(2) Do the operational test of the cockpit door lock syst

refer to AMM 52-51-00 Page block 501

.

1 cable tie Item (2

1 plug cover Item (2

2 screws with

clamps

Item (2

1 cover Item (2

2 screws Item (2

1 wire protection F2527496220200 Item 8

4 screws NAS1102-08-6 Item 7

4 washers DAN125-4 Item 6

4 screws NAS1096-2-10 Item 12

8 washers NAS1149CN832R Item 14

4 clamps MS21919WCH7 Item 11

4 nuts MS21042L08 Item 13

PANEL DESIGNATION FIN LOCA

722VU CKPT DOOR LATCH 1MQ 39 V

19
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

.

(5) Do the operational decompression test on the control 

refer to AMM 52-51-00 Page block 501

.

D. CLOSE UP

(1) Make sure that the work areas are clean and clear of 

other items of equipment.

(2) In the cockpit, install the cover panels 221AC (Refe

06-41-53 Page block 001 and AMM 25-23-42 Page block 4

(3) In the cockpit, install the ceiling and sidewall pan

(Refer to AMM 06-41-53 Page block 001 and AMM 25-13-4

401).

(4) In the cockpit, install the Anti Hijack Camera, refe

23-72-51 Page block 401.

(5) In the cockpit, on the overhead panel, install all t

plates necessary to get access to the modification of 

and wiring.

(6) Remove the warning notices.

(7) Close the passenger/crew door 831 (Refer to AMM 52-10

201).

(8) Remove the access platforms.

(9) Disconnect the aircraft electrical ground connection 

12-34-24 Page block 201).

E. DOCUMENTATION

Write in the applicable aircraft records that you have don

given in this Service Bulletin.

20
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 1

Removal of the Electrical Harness 7450VB

21
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This Page Intentionally Left Blank

22
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 2 (Goto A3 section)

Removal of the Electrical Harness 7450VB

23
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 3

Removal of the Electrical Harness 7450VB

25
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 4

Removal of the Electrical Harness 7450VB

26
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 5

Removal of the Electrical Harness 7450VB

27
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 2 Sheet 1

Removal of the Cockpit Door Panel

28
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 2 Sheet 2

Removal of the Cockpit Door Panel

29
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 3 Sheet 1

Modification of the Cockpit Door Panel

30
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 3 Sheet 2

Modification of the Cockpit Door Panel

31
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 4 Sheet 1

Installation of the Cockpit Door Panel

32
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 4 Sheet 2

Installation of the Cockpit Door Panel

33
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 1

Installation of the Electrical Harness 7450VB

34
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 2 (Goto A3 section)

Installation of the Electrical Harness 7450VB

35
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 3

Installation of the Electrical Harness 7450VB

37
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 4

Installation of the Electrical Harness 7450VB

38
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 5

Installation of the Electrical Harness 7450VB

39
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 6

Installation of the Electrical Harness 7450VB

40
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 7

Installation of the Electrical Harness 7450VB

41
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This Page Intentionally Left Blank

42
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 6 Sheet 1 (Goto A3 section)

Wiring of the Electrical Harness 7450VB before Accomplishment of 

43
DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 7 Sheet 1 (Goto A3 section)

Wiring of the Electrical Harness 7450VB after Accomplishment of S

45
6 DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

A - SB WILL BE embodied............. YES/NO (if NO p

If YES, aircraft concerned (as per SB effectivity by default) and 

(month/year) of embodiment:...................

.................................

.................................

B - SB HAS BEEN embodied on aircraft:..............

.................................

.................................

Operator comments:.......................

................................

................................

From Airline:..........................

Name/Title:...........................

Signature:.............. Date:......

If operational documentation is affected (see Paragraph 1.K of th

information is needed prior to next normal revision or prior to S

please indicate required service(s):

Either: Advance Data..................... YE

Or : Intermediate/Temporary revision............ YE

Important Information: This SB will only be incorporated in your m

operational documentation if this sheet is returned to Airbus and 

duly authorised representative. With the next feasible revision, 

result in

- updating of maintenance documentation to show pre and post S

- updating of maintenance and operational documentation to show 

after embodiment.

If this SB requires previous or simultaneous accomplishment of ot

Airbus shall automatically include them in the manual revisions. 

00-037 for detailed information.

Please return this completed sheet to:

 AIRBUS

 CUSTOMER SERVICES DIRECTORATE

 1 Rond Point Maurice Bellonte

 31707 BLAGNAC CEDEX FRANCE

 Attn: SDC32 Technical Data and Documentation Services

 FAX: (+33) 5 61 93 28 06

 or via your Resident Customer Support Office.

 Alternatively, SB lists via letters or fax are also accepted.
6 DATE : Oct 12/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Apr 25/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(Please rate on a scale of 1 to 4, with 4 being the 

- Quality rating of this SB 

- Quality rating of the Accomplishment Instructions 

- Quality rating of the Illustrations 

- Is this SB easy to understand ? 

If you have had difficulties in the accomplishment of this SB plea

the area(s) and give a short description of the issue.

Planning Material Instruct

X Effectivity X Kit content X Preparat

X Reason X List of Materials X Mod/Insp

X Manpower Operator Supplied X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustra

Comments :

Operator : Date:

Name/Title :

Please return this form to :

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC

Attn : SET1 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.
@ A340

SERVICE BULLETIN

DATE : Oct 12/04 SERVICE BULLETIN No. : A340—25—4217REVISION No. : 01 — Apr 25/05 Page : 23/24

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 2

Removal of the Electrical Harness 7450VB
@ A340

SERVICE BULLETIN

DATE : Oct 12/04 SERVICE BULLETIN No. : A340—25—4217REVISION No. : 01 — Apr 25/05 Page : 35/36

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 5 Sheet 2

Installation of the Electrical Harness 7450VB
@ A340

SERVICE BULLETIN

DATE : Oct 12/04 SERVICE BULLETIN No. : A340—25—4217REVISION No. : 01 — Apr 25/05 Page : 43/44

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 6 Sheet 1

Wiring of the Electrical Harness 7450VB before Accomplishment of SB A340-25-4218
@ A340

SERVICE BULLETIN

DATE : Oct 12/04 SERVICE BULLETIN No. : A340—25—4217REVISION No. : 01 — Apr 25/05 Page : 45/46

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 7 Sheet 1

Wiring of the Electrical Harness 7450VB after Accomplishment of SB A340-25-4218