# ~A340 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellante 31707 BLAGNAC CEDEX 

### FRANCE Tel: (33) 5 61 933333 Telex AIRBU 530526F Fax: (33) 5 61 93 42 51

This summary is for information only and is not approved lor modification of the aircraft. ATA SYSTEM: 25 

### TITLE; EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR INone MINOR 1200344050120 I I 

### I

As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASONfDESCRIPTION/OPERATIONAL CONSEQUENCES The A340 aircraft in-service experience has shown that cockpit door installation must be improved. This Service Bulletin recommends to modify the cockpit door installation by adding springs and adhesive tapes on the door frame. Accomplishment ofthis Service Bulletin will improve the cockpit door reliability. GENERAL EVALUATION 

# I EVALUATION 

## ifABLE COMPLIANCE RECOMMENDED CANCELS INSPECTION SB 

### NO POTENTIAL AD 

### NO AIC OPERATION AFFECTED 

### NO RELIABILITY AFFECTED 

### YES PAX COMFORT AFFECTED 

### NO COST SAVING 

### NO LROPS AFFECTED 

### NO STRUCTURAL LIFE EXTN 

### NO VENDOR SB INVOLVED 

### NO MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER PRICE PER MAIN PARTS 

### AlC A/C (USO) Component COMPA01 1 See S8 Springs

5 DATE: Sep 21/09 SERVICE BULLETiN No_:A340-25-4326 REVISION No.: 00 -Sep 21/09 Page. 1 Printed in FRANCE (i) AIRBUS'S.A.S. 2007. All rights reserved.

# ~A340 SERVICE BULLETIN 

### SUMMARY EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) : 

### 47W 56W AAW AFR ALK ARG B3R CAL CCA CES CPA OGA OLH FIN GFA HFY IBE KAC LAN LHT M3R MAU MPO MSR NMB OAL PAL OAF R3L RJA S3R SAA SAS SVW SWR TAP THT THY UAE VCV VIR XAX CONCURRENT REQUIREMENTS None REFERENCES I REPERCUSSIONS 

### TFU None 

### DEB None 

### AOT None 

### SIL Non.e LINE MAINTENANCE AFFECTED 

### No LIFE LIMIT 

### None OTHER None NATURE OFTHE WORK AIRCRAFT 

### YES EQUIPMENT NO HARD 

# Nol SOFT 

# Nol OBRM 

# Nol MANPOWER Task2543~6·~31·801·001: Modifjc~tion TOTAL MANHOURS 1 2.00 ELAPSED TIME (HOURS) I 2.00 PENDICES pendix - Elapsed Time Assumption 

### AP Ap

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 - Sep 21109 Page: 2 Printed in FRANCE 

### eAIRBUS SAS. 2007. All rights reserved.

# ~A340 SERVICE BULLETIN SUMMARY
**CONF ALL 2220 

# /

Figure A-FSAAA - Sheet 01

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No : 00 - Sep21/09 Page:3 Printed in FRANCE © AIRBUS SAS. 2007. All rightsreserved.**CONF ALL 

# ~A340 SERVICE BULLETIN SUMMARY

I 

# ~@]
Fi9J 

### e A-FSAAA - Sheet 02 SPRING TO BE ADDED



### 5 DATE: Sep 21/09 REVISION No.: 00 - Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 Page: 4 ©AIRBUS SAS. 2007. All rights reserved.

# $A340 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DtRECTORA TE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX 

### FRANCE Tel: (33)561 933333 Telex: AIRBU 530526F Fax: (33)5 61 934251 AlA SYSTEM:25 

### TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR MODIFICATION No.: 200344D50120 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the propertyof AIRBUS, no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than thaI lorwhich it is herebydelivered. Itshall notbedisclosed inwhole orin parttothird partiesandshall n01be duplicated in any manner (exceptfor the purposesof performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein). without AIRBUS priorwritten consent. 1. PLANNINGINFORMATION "CONF ALL A. EFFECTIVITY This Service bulletin is only applicable to aircraft on which the modified

intrusionandpenetration resistantcockpitdoor is installed. (1) Models 340~211 340-212 340-213 340-311 340-312 340-313 (2) Effectivityby MSN 0002-000900110013-00150018-00290031-0035 0038-0041 0043-00440046-0049 0051-0053 0056-00580061 00630074-00760078-0081 0084-00850088-0091 0093-0094009701010103-01040114-011501170123 0125·0126 0128-01290131 0133-013701390141-01420145-01470149-01520154 0156-01610163-0164 0166-01700173-01760178-018001820185-01870190 0192-01940196-01970199 0201-020202040207-020802100212-02180220-0221 02250227-02280233 0235-0~37 02390242-02430245-02460252025702600263-026402680270 0273-0274027802800282029202970302030403070310 0318-031903210325 032703290331-03320335034703520354-035503590363 03670373-0374 0377-0379038103850387039003950399040204060411 0413-04150424 0429-04300433-0435043804420446-04470450045904670470 047404830528 05380541 0544-05460554055605590561-05620582 05850590059806430646 0651 0668 07930800083508440921 09380955

5 DATE:Sep 21/09 SERVICE BULLETIN No
..A340-25-4326 REVISION No.: 00 - Sep 21/09 Page: 1 Printed in FRANCE ©AIRBUS SAS. 2007. All rights rese",ed.

# ~A340 SERVICE BULLETIN (3) EffectivitybyOperator The OperatorlMSN relationship is provided for information only and is correcl at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer 01an aircraft from one operator to another will not be reflecled in this list unless the Service Bulletin is revised foranother reason. OPERATOR 

# , MSN 47W 0009 

### S6W 0015 

### AAW 0151 

### AFR 002900490078008401680174018602070210023702450246

026003070310031903730377 0399 

### ALK 0032 0033 0034 0367 0374 

### ARG 0048 0063 0074 0080 0085 0093 

### B3R 0046 

### CAL 0402 0406 0411 0415 0433 0541 

### CCA 019201990201 024202430264 

### CES 01290131 0141 0161 0182 

### CPA 0123 0126 0128 0136 0137 0142 0147 0157 0160 0208 0218 0220

0227 0228 0381 

### DGA 00750081 

### DLH 002000240027002800350052005300560135 015B 0213 0233

0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0355 0379 0390 0434 0447 

### FIN 0058 0835 OB440921 0938 

### GFA 0039004000970103013302120215 02B20554 

### HFY 0117 

### IBE 0005 OO~B 0125 0134 0145 0146 0170 0193 0197 0217 0221 0302 031803290332037803870414045904740483 

### KAC 0089 OO~O 0101 0104 

### LAN 0167 03$9 0363 0429 0442 

### LHT 0274 I 

### M3R 0061 I 

### MAU 0076 00Q40152 0194 0268 0793'0800 

### MPD 000700j3 MSR 015601$90178 

### NMB 00470051 

### OAL 0235 0239 0280 0292 

### PAL 0173017601870196 

### OAF 00260528 

### R3L 0004 , 

### RJA 0014 0022 003B 0043 

### S3R 0204 

### SAA 000600080011 001800190021 0544 0582 0590 0643 0646 0651 

### SAS 0413 0424 0430 0435 0450 0467 0470 

### SVW 0955
5 DATE: Sep 21109 SERVICE BULLETINNo.:A340-25-4326 REVISION No.:00 -Sep21IU9 Page:2 Prinled in FRANCE () AIRBUS S.A.S. 2007. All righls reselVed.

# ~A340 SERVICE BULLETIN ()PER~T:Q!:l SWR TAP 

### THT THY UAE VCV VIR 

### XAX 'MS~

0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 0585 0598 0041 0044 0079 0091 

## I 0385 0395 0438 0446 0668 0023 0025 0057 0115 0180 0216 0257 0270 0331 01390149 0163 0166 0185 0190 0202 0236 0031 

## I 0002 0003 0114 0164 0214 0225 02730278 (4) Configuration by MSN



### , ' MSN',{c,·'" 0002 0003 000i!-0005 0006 0007 0008 OD090011 00130014 0015 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 0031 0032 0033 0034 0035 0038 0039 0040 0041 0043004400460047004800490051 0052005300560057 00580061 00630074007500760078007900800081 0084 00850088008900900091 00930094 0097 010101030104 0114 0115 0117 0123 0125 0126 0128 0129 0131 0133 0134 0135013601370139014101~01~01~014701~0150 015101520154015601570158015901600161 01630164 01660167016801690170017301740175017601780179 018001820'185018601870190 '01920193019401960197 01990201 020202040207020802100212021302140215 02160217021802200221 022502270228023302350236 023702390242024302450246025202570260 02630264 02680270027302740278028002820292029703020304 030703100318031903210325032703290331 03320335 0347035203540355035903630367037303740377 0378 03790381 03850387039003950399040204060411 0413 04140415 04240429043004330434043504380442 0446 0447045004590467047004740483052805380541 0544 05450546055'4055605590561 0562058205850590 0598 064306460651 066807930800083508440921 09380955 (5) Configurationdefinition 

### "CONFIGJj XA110~1 001

dCONF 001 Config. 001 isvalidforalltheaircraftgiven inthe effectivityofthisService Bulletinasa standardconfiguration. (6) Material Effectivity 

### fOIATERIi':(w 

## 'ilil ,;",,"~".~' '+'N;. •,Q;T.l!!f'E~?Ii!(Dli? 

## SSfu~~$i'%'+

" "," ,"t, •.-' "'" ". ,'" ~ ComponentCOMPAOl 1 ConsumableC'MLAOl 

### As required B. CONCURRENT REQUIREMENTS 

### None 5 DATE:Sep 21/09 SERVICE BULLETIN No.:A340-25-4326 REVISION No.: 00 - Sep21/09 Page:3 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reseiVed.

# I~A340 SERVICE BULLETIN 

## c. REASON (1) Hislory The A340 aircraft in-service experience has shown that cockpit door installation must be improved. (2) Objective/Action This Service Bulletin recommends to modify the cockpit door installation by adding springs and adhesive tapes onthe doorframe. (3) Advantages I Accomplishment of this 

# serce Bulletin will improve the cockpit door reliability. (4) Operational/Maintenance Consequences None 

### D. DESCRIPTION Toaccomplishthis ServiceBulletin it is necessaryto : Task 254326-831·801-001: Modification (1) Installthe Springsonthe Strikeofthe Cockpit Door. E. COMPLIANCE (1) Classification RECOMMENDED

APPROVAL F. (2) Accomplishment Timescal,

Accomplishmentof this ~ervice Bulletin is where manpowerandfacilitiesare available. I recommended at the earliest opportunity
Approved under EASADesignOrganisationApproval No. EASA21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content 01 this Service Bulletin, the operator is responsiblefor obtainingapproval by its airworthinessauthority lor any adaptation necessary before incorporationofthe ServiceBulletin.

5 DATE:Sep 21/09 SERVICE BULLETINNo.:A340-25A326 REVISIONNo.: 00 -Sep21109 Page:4 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reseNed.

# ~A340 SERVICE BULLETIN
G. MANPOWER The manpower estimates given in this Service Bulletin are based on ·the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards 10suit operator's circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying limes for paints, sealants, elc., and general administration work are also not included.

0.50 0.50 0.50 2.00 2.00 

### ,j:Hil{','2~26~8S'f~80i~oO'1:-



## r¥1:o jftPJi)10 0.50 Gel Access 

### On Aircraft Install the Springs on the Strike 01the Cockpit Door. 

### Tesls Close-Up TOTAL MANHOURS ELAPSED TIME (HOURS)

For detail concerning the elapsed time assumption, refer to Appendix
. Elapsed Time Assumption. H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed 

### J. REFERENCES Aircraft MaIntenance Manual (AMM) 1234-24 20·21·11 52·10-00 52-51-11 Consumable Material List (CML) Elec. Std Practices Manual (ESPM) 20-55-00 Structural Repair Manual (SRM) 51-42-00 K. PUBLICATION AFFECTED IlIlustrated Parts Catalog (lPC) L INTERCHANGEABILlTV/MIXABILlTY 

# I 52-51-01

Not Applicable M. SPARES None



### 5 DATE: Sep 21/09 SERVICE BULLETIN No,: A340·25-4326 REVISION No : 00 - Sep 21/09 Page: 5 Prinled in FRANCE © AIRBUS SAS. 2007. All rigl1tsreserved,

# ~A340 SERVICE BULLETIN

This Page Intentionally Left Blank

5 DATE: Sep 21/09 REVISION No.: 00 - Sep 21/09 Printed inFRAiCE SERVICE BULLETIN No.: A340-25-4326 Page: 6 ©AIRBUS SAS. 2007. All righls reserved.

# ~A340 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAilABILITY (1) Procurement Addresses This Service Bul,letin is the subject ot an AIRBUS monitored retrofit campaign. Component COMPA01

(2) Priceand Availa'bility NoAIRBUS kitwill be provided. Customers with aircraft shown in the effectivity of this Service Bulletin should send a purqhase order to AIRBUS. Quote the number 01this Service Bulletin. The address is: Airbus Spares Support and Services Weg beim jaeger 150 0-22335 Hamburg Germany For ordering by internet: http://spares .airbus.com Forordering by fax: +49.40.50,76.25.90

Parts required to accomplish this Service Bulletin can be manufactured by the operator following the Fig. A-FBBAA or ordered by aspares purchase order to AIRBUS. 

### B. INDUSTRY SUPPORT INFORMATION Forthe organisation ofthis retrofit, operators are kindly requested to contact AIRBUS retrofit management department. AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellante 31707 BLAGNAC CEDEX France Tel. (33)5 67190622 E-mail: monitored.retrofit@airbus.com Fax
. (33) 5 61 93 27 45 Parts are at no charge forthe operator. The man-hours indic1ted inthis Service Bulletin will remain at the operators' cost. C. LIST OF COMPONENTS No Kit

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 - Sep 21/09 Page: 7 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reserved.I

# ~A340 SIERVICE BULLETIN D. LIST OF MATERIALS M OPERAifOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ,I~~GE$'GRIPTION A'·' i'4ii Solvent General Purpose Adhesive tape (2) Components As required 

### '1M) SEE " '

N,bTES '

Component COMPAQ1 dT~MNE~~T 1 1183387

(3) Equipment None E. PARTS TO BE RE-IDENTIFIEDI BY OPERATOR 

### None F. TOOLING None 

# .ARTN.

I

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-26-4326 REVISION No.: 00· Sep 21/09 Page: 8 Printed in FRANCE © AIRBUS SAS. 2007, All rights reserved.

# $A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 254326-831-801-001 - Modification WARNING.

### Q,A.I)JIONMAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES. ALWAYS OBEY THE PRECAUTIONS THAT FOLI.OW TO KEEP ELECTRICAL WIRiNG IN A SATiSfACTORY CONDITION (ELEGTRIC,c.,Ll Y AND MECHANICALLY SERV]CEA3LEi WHEN YOU 00 MAINTENANCE WORK. REPA!RS OR MODIF1CATJONS.ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AMEAAS CLEAN AS POSSiBLE TO DO THIS' PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC: AS NECESSJ!.RY ON WIR!NG AND COMPONENTS. REGULARLY REMOVE ALL SHAViNGS, UNWANTED r>.1ATERiAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATiON AND DAMAG TO THE ELECTRICAL, WIRING INSTALLATION, If'-JCASE OF CONTAMINATION REFER TO ::'SPM 20-55-00 Task Associated Data

• > Zon.e 

# , 210 220

. 

## " Access:, Door 1831 c 

# , Manpow§!'r 

# ''''. . 

# "' TOTAL MANHOURS 12.00 ELAPSED TIME (HOURS) 12.00 A. GENERAL (1) Subtask 254326-910-001-001 - Standard Practices



## . Skills 

# . - Manpower Resources INON SPECIFIC Material necessary to do the job Consumable CMLAOl ITEM ,J;>ESCRIPTIONJ, REF~RENCE TO OLX PER 

### MC SEE



### ~ ..!l£ CMUMAT.N<:l. NOTES Solvent General Purpose 11-026 As required

5 

### fji Aircraft Maintenance Manual (AMM) DATE: Sep 21/09 

## Refereti®s Task 20-21-11-911-801

SERVICE BULLETIN No_:A340-25-4326 REVISION No.: 00 - Sep21109 Page: 9 Printed in FRANCE () AtRBUS S.A.S. 2007. All rights reserved.

# $A340 SERVICE BULLETIN

(Mat. No.), refer to Consumable I 

### 5"'2,00 I material numberk of the (a) For the specification Malerial List (CML). w 

# ~i~"".~''''- \< I ~*~)pJ:<.lere'lce_S-<N: j't11\- Consumable Material List (CMl) Structural Repair Manual (SRM)
(b) Cleantheworkareawith:


### ~~~~~:~ Geeecal 

# T26 As 

### Ticed (c) For the removal and installation of fasteners (Refer to SRM 51-42-00). (d) To torque tighten the standard threaded fasteners (ReIer to AMM Task 20-21-11-911-801). 

# I (2) Subtask 254326-839-001-001 -Administrative 

## ~anp:o~l!'l~];urc~'~, Skills Write in the applicableaircraft recordsthat you have done all the work given in this Service Bulletin. B. PREPARATION 

## I (1) Subtask 254326-941.001-0f' -Job Set-up O®~OhEfs'and'Accessd:'aflel~ ",,'-



### :0,P.:cce.ssJWork:

Jo.catlQiX"·"' I I I SkHls

~ Refe'renGes
.. ""..,- Aircraft Maintenance Manual (AMM) Task 12-34-24-8160-802 I Task 52-10-00 0110-801 (a) Make sure that 

# thJ aircraft is electrical

# I) grounded (Refer to AMM Task 12-34-24-860-802). I (b) Putaccess platform i1 position I (e) Open the passenger/crew door 831 (Referto AMM Task 52-10-00-010-801).

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 - Sep 21/09 Page: 10 Printed in FRANCE © AIRBUS $AS, 2007. All rights reserved.SERVICE BULLETIN
C. PROCEDURE (1) Subtask 254326~831~001-001
- Install the,Springs on the Strike ofthe Cockpit Door. }lZone~ 210 220 Access 

## 1l' 

# I Manhours Minimum number of person Subtask elapsed time Skills

Fig.A-FBAAA

Fig.A-FBBAA 

## ork"ZoneS:'aiId ,;Ceess'Pa6els' ~,
, '",,'~cQe:~s7.Woti<:Jocation'.* Door 831
0.50 1 

### 0.50 AIRFRAME



### R'ef '8 aEt§'· Sheet 01 - Installation of Springs on the Strike ofthe Cockpit Door Sheet 02
. Installation of Springs on the Strike ofthe Cockpit Door Sheet 03 - Installation of Springs on the Strike ofthe Cockpit Door Sheet 01 - Principle of Manufacture ofthe Springs

6
3

6 (a) Remove:

Screw (b) Install: Spring 1183387 and attach with : Screw Item (2)
Item 1
Item (2) Retain

Retained at removal

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 -Sep 21/09 Page: 11 Printed in FRANCE © AIRBUS B.A.S. 2007. All rights reserved.

# ~A340 SERVICE BULLETIN The springs item 1 can be ordered by a spare purchase order 10AIRBUS or manufactured by the operator following the ~ 

# FBB4 Sheet 01, 

# I (e) Apply on the door the :Adhesivetape on all surface in contact between the door and the springs item 1. I Adhesivetape DAN269~25 1 (M) D. TEST (1) Sublask 254326-700-001-001
. Testing

Door 831 Access I 

# ''''''~''ltorki~~'s

:~~" cces;s.P.an~f~~~>,' 

# 'Zone . ;pi

### "S~cpes;S!Work IOC?1tl 210 220
Skills 

## M,anlicrwe:r ReoolJ£;5' I I U 

# :*, ,iIiB~er"'~'"s j Aircraft MaintenanceManual (AM~) Task52-51-11-8?0-801 {al Check that the COCkPiJ door operates properly 

# dy opening/closing it several times. If the door is fOU~d hard 10open (or 

### closel, do the adjustment of the door gap (Refer to AMM Task 52-51-11-820-801). E. CLOSE-UP (1) Subtask 254326-942-001-001
. Close-up



### ~; It Aircraft Maintenance Manual (AMM) I AIRFRAME I 

### c~f~s 

# !: c, .. Task 52-10-00-410-801

I

. o®:~and'fi:.ct;ess,· Panels'

AcC'---~2Wdrk;lo' ~ion_ I I I 

## ~~npow-e.f 

# ResJ2Ur~._ I I Skills

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment (b) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801) (c) Remove the access platform. (d) Restore the systems Jnd the aircraft to normal ,operating condition. 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No: 00 - Sep 21/09 Page: 12 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reserved.

# $A340 SERVICE BULLETIN

*-CONF ALL 2220 

# /

5 DATE: Sep 21/09 FigureA-FBAAA - Sheet 01 Installation of Springs on the Strike ofthe Cockpit Door SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 - Sep 21109 Page: 13 Prinled In FRANCE 

### eAtRBUS S.A.S. 2007. Allrights reserved.I

# I~A340 SERVICE BULLETIN

HCONF ALL 

## BEFORE

(2)

Figure A-FBAAA -Sheet 02

Installation of Springs on the Strike ofthe Cockpit Door
5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 - Sep 21/09 Page: 14 Printed in FRANCE @AIRBUS S.A.S. 2007. All r;ghls reserved.

# ~A340 SERVICE BULLETIN

**CONF ALL

(2)

APPLY ON THE DOOR THE ADHESIVE TAPE DAN 269-25 ON ALL SURFACE IN CONTACT BETWEEN THE DOOR AND THE SPRINGS,

COCKPIT DOOR



## ~ A-A

5 DATE: Sep 21/09 Figure A-FBAAA - Sheet 03 Installation of Springs on the Strike of the Cockpit Door I SERV1CE BULLETIN No.: A340-25-4326 REVISIONNo:00- Sep21/09 Page: 15 Printed in FRANCE 1)AIRBUSSAS. 2007. All rights reserved.

## i$A340 SERVICE BULLETIN

"CONF ALL PRINCIPLE OF MANUFACTURE 

# Ai

,~ (0.079110) 101"11"1 (0,3941"1 1,01"11"1 (0.0751101 

# r-: ~ 37' 100'(
-- f 21.81"11"1 .7mm? (0,858 in) 1144841101 152~I...J (o31~8~nl--l

154 le8mm

(0654 In) 

# , . R. 10

### n"" ,10.394In)

,DIAM. 9.91 mm

# I (0.390In), 

# I-~; ~ -I 

# --i?B:I 1,
..... (O.9~5Inl 

# tl - ~-


# -~- -~~-+ 10 mm 0.31"11"1 (0.394~nl (0,0121101 

## ~~--. -~-~-~-~-~-~ 

## I 

# A..J "- (0.7571"1 DIAM. 5.62 mm (0.229 in)

• 83,5 mm (2.500 In) A-A

IlIATEfllAL ASNA3322 OR AMS55180R \.4319

F_S9_25~326_5_BBM,..O 1_02 THICKNESS 0,4m"'(0,157Inl IDENTIFICATION IOENl1FV THE SPRING WITH PART NUMBER 1183387 NOTE: NOT SPECIFIED RADIUS, R. 3......, (0,118 inl 40,2 mm 1I.883In)

'mm (0.197 In) 'mm (0.19710) ~I 

# ,

# ..._(/ ~' (0.016110) _~_



# "'-'mm-=- 

# I p.2871nl •• UNFOLD 

# -----1-1---

, 25m01 

# !(0,98'1101

101"11"1 {O.394In) 

### ~.,

, A. 0.75 mm

- - -) (0,02910) 1 30.2mm 11.180 in)

Figure A-FBBAi\. Sheet 01 Principle al Manulactura of Ihe Springs 

# , DATE: Sep 21109 SERVICE BULLETIN No.:A340-25·4326 REVISION No.: 00· Sap 21109 Page: 16 P';O'.dInFRANCE e AIRBUS B,A.S, 2U01.Al"""10 r.",.wd.

# ~A340 SERVICE BULLETIN Appendix - Elapsed Time Assumption
hCONF ALL

ELAPseD TIME ASSUMPTIONS SERVICE BULLETIN No. A340-25-4326

(HOURS) 2.0 2.0 TOTAL MANHOURS 

## (MHll ELAPSeD TIME (El) STEPS MH 

### ET PER

GET ACCESS 0.50 0.50 1 I

SPRINGS INSTALLATION 0.50 0.50 1 

### I I


### TEST 0.50 0.50 1 

### I I
CLOSE-UP 0-50 0.50 1 

### I I

1 I I I 0 0.5 1 1.5 2 ELAPSED TIME

MH: MANHOURS ET: ELAPseD TIME PER: NUMBER OF PERSONS NOTE; THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM.

Figure A-FAAAA - Sheet 01 Appendix - Elapsed Time Assumption
5 DATE: Sep 21109 SERVICE BULLETIN No.: A340-25-4326 REVISION No : 00 - Sep 21109 Page: 1 Printed in FRANCE €:IAIRBUS SAS. 2007. All rights reserved.

# ($;A340

TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IM1ROVE COCKPIT DOOR MODIFICATIONNo.: 200344050120 Please complete the appropriate item (Aor B): I A - S8 WILL BE embodied I YES/NO (If NO please comment) If YES, aircraft concerned (as per S8 effectivity by default) dnd planned dates (month/year) of embodiment:

B - S8 HAS BEEN embodied on aircraft: Operator comments:
From Airline: NamelTitle: Signature: Dale:

YES/NO YES(NO If operational documentation is affected (see Paragraph 1.K of this S8): II information is needed prior to next normal revision or prior 10S8 embodiment, please indicate req1uiredservice{s): Either: Modification Operational Impact (MOl), if available Or : Intermediate revision Important Information: This S8 will only be incorporated in your maintenance and operational documentation if this sheet is returned to IIAi'bUSand signed by a 'duly autho,ised cep,esentati,e. With the next feasible revision, this will result in I

- Updating of maintenance documentation to show pre and post 58 data.

- Updating of maintenance and operatioral documentation to shQw post 5B data after embodiment. If this S8 requires previous or simultaneous accomplishment 01 d~her SBs, Airbus shall automatically include them in the manual revisions. ReIer to SIL OO~037for detail~d information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Belionle 31707 BLAGNAC CEDEX FRANCE Attn. SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 932806 I e-mail. sb.reporting@airbus.com or via your Resident Customer Support Office Alternatively, SB lists via letters or fax are ::1lsoaccepted.

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No: 00 - Sep 21/09 Page: 1 Printed in FRAN9E © AIRBUS SAS. 2007, f\11rights reserved.

# $A340 SERVICE BULLETIN QUALITY PERCEPTIQN FQRM Use this form to tell us what is your perception of the quality ofthis Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rale on ascale of 1 to 4, with 4 being the highest score)

- Quality rating ofthis S8

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If you have had difficulties inthe accomplishment ofthis S8 please quote below the area(s) and give a short description 01 the issue Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Name/Title: Please return this form to AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellante 31707 BLAGNAC GEDEX FRiNGE Attn : SEM4 Service Bulletins Management FAX: (33) 5 61 934251 Orviayour Resident Customer Support Office. Date:

5 DATE. Sep 21/09 SERVICE BULLETIN No.: A340-25-4326 REVISION No.: 00 - Sep 21/09 Page: 1 Printed in FRANCE © AIRBUS' S.A.S. 2007. All rights reserved.