# ~A340·500/600 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)561 934251 This summary isfor information only and is notapproved for modification ofthe aircraft AlA SYSTEM: 25 

### TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR *-CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 

## INone MINOR 

### [200344050120 

## I I I I NOTE: As per EASA IR 21, a minorchange is one thai has no appreciableeffect on the

mass, balance, structural strength, reliability. operational characteristics affecting the airworthiness ofthe product. All other changes are major changes. REASON/OESCRIPTIONfOPERATIONAL CONSEQUENCES The A340-500/600 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 

### EVALUATIONITABLE COMPLIANCE RECOMMENDED CANCELS INSPECTION SB 

### NO POTENTIAL AD 

### NO NC OPERATION AFFECTED 

### NO RELIABILITY AFFECTED 

### YES PAX COMFORT AFFECTED 

### NO COST SAVING 

### NO LROPS AFFECTED 

### NO STRUCTURAL LIFE EXTN 

### NO VENDOR S8 INVOLVED 

### NO MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET OTY PER PRICE PER 

# I MAIN PARTS 

### Ale AIC (USD) Component COMPA01 1 See SB 

## ISprings


### 5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No: 00 - Sep 18/09 Page: 1 Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.

# ~A~~~;~~?~600

SUMMARY EFFECTIVITY This Service Bulletin is applicable to this (t

# I 8Se)operator(s) : 62X 72W 79W ARA CES CHH DLH ETD HFY IBE SAA SIA TAM THA UAE VIR KFR QAF OIR CONCURRENT REQUIREMENTS None REFERENCES I REPERCUSSIONS TFU 

### None OEB 

### None AOT Non~ SIL 

### None LINE MAINTENANCE AFFECTED No 1 LIFE LIMIT 

## None OTHER 

### None NATURE OFTHE WORK AIRCRAFT YES! EQUIPMENT NO 

## 1 , HARD NO 

## 1 SOFT NO 

## 1 1 OBRM NO 

## 1 MANPOWER Task,255:H39~831~8Q-1·001: Modifica,'tion TOTAL MANHOURS 

## 1 1200 ELAPSED TIME (HOURS) 

## 1 12.00 PENDICES pendix - Elapsed Time Assumption

DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No.: 00 - Sep 18/09 Page: 2 

### AP

5 

### Ap

# ~A340·5001600 SERVICE BuLLETIN SUMMARY
HCONF ALL

Figure A-FSAAA - Sheet 01 Z220 

# /

5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISIONNo
.. 00 - Sep 18/09 Page:3 Printed in FRANCE 0 AIRBUS SAS. 2007. All rights reserved.I 

# ~A340·500/600 SIERVICE BULLETIN SUMMARY
**CONF ALL

I



# ~@]
Figut A-FSAAA - Sheel 02 SPRING TO BE ADDED

5 DATE: Sep 18/09 REVISION No.: 00 - Sep 18/09 SERVICE BULLETIN No,; A340-25-5169

© AIRBUS SAS. 2007. All rights reserved.SERVICE BULLETIN AIRBUS CUSTOMERSERVICES DIRECTORATE 1 Rond PointMaurice Bellonte 31707 BLAGNACCEDEX FRANCE Tel. (33)5 61 933333 Telex: AIRBU 530526F Fax: (33)561 934251 ATASYSTEM:25 

### TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR MODIFICATIONNo.: 200344050120 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of 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 informationcontained in it shall betreated asconfidential, shall notbe usedforany purposeotherthan thatforwhich itis herebydelivered. Itshall notbedisclosedin wholeorin parttothird partiesandshali notbe duplicated in any manner(exceptfor the purposesof performingthe tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS priorwrittenconsent. 1. PLANNING INFORMATION HCONF ALL A. EFFECTIVITY This Service bulletin is only applicable to aircraft on which the modiHed

intrusionand penetration resistantcockpitdooris installed. (1) Models 340·541 340-542 340-642 (2) Effectivityby MSN 0371037603830391 039404100416-04170426043104360440044504490453 0457046004640468 0471 04750478048204850488 04920495049905140517 052005230531 0534 05370540054305470557 0560056305660569 05720575 0577058005830586 06010604060606080611061506170619062206240626 0628063006390672 06770681068506890694069807020706071007150719 072307270736074007440748075307570761-07680771 0775077907830787 079007940798080408120829083708460848 0870 DB860894089709020910 0912091709240929093309530972 09810987 0993 1005 1030 1040 (3) EffectivitybyOperator The OperatorlMSN relationshipis providedfor informationonlyand is correctatthetime of issue in accordance with the information available to AIRBUS. Any fulure changes resultingfrom transferof an aircraftfrom one operatorto anotherwill not be reflectedin this listunlessthe ServiceBulletin isrevisedforanotherreason. 5 DATE:Sep 18/09 SERVICE BULLETIN No.:A340·25-5169 REVISION No.: 00- Sep 18/09 Page: 1 Printed in FRANCE (l AIRBUS S.A.S. 2007. All rights reserved.SERVICE BULLETIN


### OPERATOR ~ 

## 1 MSN 62X 0779 72W 0917 79W 0924 

### ARA 09100912 

### CES 0468048805140577 0586 

### CHH 0436 0453 0475 

### DLH 0482 0517 0523 0537 0540 0543 05660569 0580 0583 07620763

07670771 0790079408120846084808970972 0981 09871005 

### ETD 074807570761 07830829083708700929093310301040 

### HFY 0894 I 

### IBE 0431 044004600601060406060.61706190672070207270744

0993 I I 

### KFA 08860902 

### QAF 0495 I 

### QTR 0715 0740 0766 0798 

### SAA 041004170426053105340547055706260630 

### SIA 0478 0492 049905600563 

### TAM 04450464 

### THA 062406280677 0681 068906980710071907750953 

### UAE 0394 0457 0471 0485 05200572 0608 0611 06850694 

### VIA 037103760383039104160449057506150622063907060723

0736 0753 07640765 0768 0787 0804 (4) Configuration by MSN I 

### MSN CONF.IGURATION 0371 0376038303910394041004160417042604310436 001 0440 0445 0449 0453 0457 046004640468 0471 0475 0478 04820485048804920495049905140517052005230531 0534 0537 0540 0543 0547 0557 05600563 0566 0569 0572 , 05750577 0580 0583 058p060106040606060806110615 061706190622062406260628063006390672 0677 0681 , 06850689069406980702070607100715071907230727 0736074007440748075307570761 0762076307640765 0766 0767 0768 0771 0775 07790783 0787 0790 0794 0798 08040812082908370846084808700886089408970902 0910 0912 0917 0924 09290933 0953 0972 0981 0987 0993 100510301040 (5) Configuration definition *·CONF 001 Config. 001 isvalid for allthe aircraft given inthe effectivity ofthis Service Bulletin as a standard configuration. (6) Material Effectivity

5 MATERIAL

Component COMPA01 DATE:Sep 18/09 REVISION No.: 00
-Sep 18/09 QTY PER NC SEE NOT~S 1 SERVICE BULLETIN No.: A340-25-5169 Page: 2 ©AIRBUS SAS. 2007. All rights reserved.SERVICE BULLETIN r;MA=T"E"R;;-,A"L--------~· 'I-'-"Q"'TY=P"E~R~N=C-'-S"E"E"N"O"TE=SO'--, Consumable CMLA01 As required B. CONCURRENT REQUIREMENTS None C. REASON (1) History The A340-5001600 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 on the doorframe. (3) Advantages I Accomplishment ofthis Service Bulletin will improve the cockpit door reliability. I (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task.255169-831-801-001: Modification
COMPLIANCE 

### E. (1) Install the Springs on the Strike ofth,eCockpit Door. 

# I (1) Classification RECOMMENDED (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL Approved under EASA Design Organisation Approval No_EASA 21J.031.

5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No.: 00 - Sep 18109 Page: 3 Printed in FRANCE ., AIRBUS S.A.S. 2007. All rights reserved.MANPOWER 

### G. I The manpower estimates given in this Service Bulletin are based on the direct labor cost 10 do the work. These estimates assume that the work wlll be done by experienced personnel, and may need to be revised upwards to suit 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 times lor paintsl,sealants, etc., and general administration work are also not included, 

# I I ."'~." II , 

### "Jli'"St'ras.~JgJ.:i'5,1!{916'3~

## ~_8olt;:(JD:t:M"6liili¢atip1'\~; ~_Y0_ Get Access I 0.50! On Aircraft I I Install the Springs on the Strikeoft~eCockpitDoor. 0.501 Tests I 0.50' Close-Up I 0.50 TOTAL MAN HOURS I 2.00 ELAPSED TIME (HOURS) I 2.00 NOTE: I

For detail concerning the elapsed time! assumption, refer to Appendix - Elapsed Time Asisumption
. H
I.

J WEIGHT AND BALANCE Not Changed ELECTRICAL LOAD DATA Not Changed REFERENCES Aircraft Maintenance Manual (AMM) 12-34!24 20-21-11 52·10-00 I 52-51-11 Consumable Material List (CML) I Elec. Std. Practices Manual (ESPM) 20-55-00 Structural Repair Manual (SRM) I 51-42jOO

52-51-10 PUBLICATION AFFECTED I IllIustrated Parts Catalog (IPC) I INTERCHANGEABILITY IMIXAJ'LlTY 

### K.
L. Not Applicable M. SPARES None 5 DATE: Sep 18/09 REVISION No.: 00 - Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 Page: 4 © AIRBUS SAS. 2007. All rights resEwed.SERVICE BULLETIN
2. MATERIAL INFORMATION "CONF ALL 

### A. MATERIAL· PRICE AND AVAILABILITY (1) Procurement Addresses ThISService Bulletin isthe subject of aniAIRBUS monitored retrofit campaign. Component COMPA01

(2) Price and Availability NoAIRBUS kitwill be provided. Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Airbus Spares Support and Services Weg beim jaeger 150 0-22335 Hamburg Germany For I ordering by internet: http://spares.airbus ,com Foro~deringbyfax: +49.40.50.76.25.90

Parts required to accomplish this Service Bulletin can be manufactured by the operator following the Fig. A-FBBAA orordered by aspares purchase order to AIRBUS. B. INDUSTRY SUPPORT INFORMATION Forthe organisation 01this retrofit, operators are kindly requested to contact AIRBUS retrofit management department AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX France Tel: (33) 5 67190622 E-mail: monitored.retrofit@airbus.com Fax: (33) 5 61 93 27 45 Parts are at nocharge torthe operator. The man·hours indicated inthis Service Bulletin will remain atthe operators' cos!. C. LIST OF COMPONENTS No Kit

5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No: 00 - Sep 18109 Page: 5 Printed in FRANCE f:I AIRBUS S.A.S. 2007. All rights reserved.I D. LISTOF MATERIALS· OPERATOR SUPPLIED , (1) Consumable Materials Consumable CMLA01 

### ITEMDESCRIRTION '

# " Solvent General Purpose Adhesive tape (2) Components Component COMPAQ1 REFERENGE'i4:0 8M MAT: Nit" ·,c. 

### '4 11-026 DAN269-25 

### nl'¥~PEfl AlOt, , SEE,



# ';!A"" , •• NOTES As required


## , 1M)

(3) Equipment 

### None E. PARTS TO BE RE·IDENTIFIED BY OPERATOR 

### None F. TOOLING 

### None

5 DATE, Sep 18/09 REVISION No.: 00 - Sep 18/09 SERVICE BULLETIN No.' A340-25-5169 Page: 6 ©AIRBUS S.A.S. 2007. All rights reserved.SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 255169·831-801-001 - Modification

PUT PROTECTION. SUeil NFCES$ARY ON WIRiNG WARNING: 

## 9A.lJJIO!\!.: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED INTHE REFERENCED PROCEDURES, I ALWAYS OBEY THE PRECAUTIONS THAT FOLlOV! TO ,{[EP ELECTRiCAL WIRING iN A SATiSFACTORY COh;DiTiOt\j RiCALL Y l\NO :vH::,CHANICALLYSERViCE.ABLE) WHE~~ YOU DD Mi\INT:J,J/\\C[~ WORK. REF'AIRSOR iVl0CJ!F:K;~TiONS,AlWAvS KEEP ELECTRiCAL W COMPONENTS AND THE \NO~K AREA AS CLEAN ,AS 

### POSSIBU:: TO 00 THiS. ! A$ PU\ST1C SHEETING, CLOTHS, ETG, AS COMPONENTS I REGULARLY REMDVF ALL SHfV!NGS. UNWANTED iv1ATERiAL,

### Nm OTHERCONTA~11blATloriTHESE PRECAUTIONS WiLL iflECREASE THE, RiSK OF CC)I<TJ,\,I\lINAT:CY,J AND DAMAGE. TO THE ELECTRH:::;AL WiRING INSTALLATION. if< CASE OF CONTAMiNATION REFER TO ESP\1 2055-00 Task Associated Data

TOTAL MANHOURS ELAPSED TIME (HO~RS) A. GENERAL 

## M,",gpvJ~' 2.00 2.00 (1) Subtask255169-910-001-001 - Standard Practices

,,W1u~Ppw_eR;He:Sourcm.:'i<'~-I,'_ NON SPECIFIC

!-

__ 

## '-?0&:-;R:ete~ndes Aircraft Maintenance(vlanual(AMM) Task20-21-11-911-801 5 DATE: Sep 18/09 SERVICE BULLETIN No. A340-25·5169 REVISION No.: 00 - Sep 18/09 Page: 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.I 

# ~A340·500/600

S~ERVICE BULLETIN I 

## R~f,e:rences '"'1',

I Consumable Material List (CML) Structural Repair Manual (SRM) (a) For the specification Material List (CML). of the I 51-42-00

material numberJ (Mat. No.), refer to Consumable (b) Cleantheworkareawith. 

### I SolventGeneral 11-026 As required Purpose I (c) For the removal and Inlstallallon of fasteners (Refer to SRM 51-42-00) (d) To torque lighten 

### tre standard threaded fasteners (Refer to AMM Task 20-21-11-911-801 ). (2) Subtask 2551-69-839-001-001 - Administrative

in this I

# INON SPECIFIC Write in the applicable air~raft recordsthat you hJve done all the work given Service Bulletin. Skills

B. PREPARATION (1) Subtask 255169-941-001-001 -Job Set-up

, 'A;Work:!:~oDe~<:!T;la Acceq ~~nel,~V' 

### :~" ;'Acce~·::;,NVciiID(oca.tion· i4% I I I 

# ,'*Ma -,;,..;; {'" I AIRFRAME I I 

## f Xa@erence_s I 

### 'w Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 I Task52-10-00-010-801 (a) Make sure that the! aircraft is electrically grounded (Refer to AMM Task 12·34-24-860-802)
. (b) Putaccess platform in position (c) Open the passenger/crew door 831 (ReIerto AMM Task 52-10-00·010-801).

5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No.: 00
. Sep 18/09 Page: 8 Printed in FRA~CE ® AIRBUS S,AS. 2007. All rights reserved.SERVICE BULLETIN



# c. PROCEDURE (1) Subtask 255169-831-001-001 - Install the Springs on the Strike ofthe Cockpit Door. ""Work Zones and A~ess panels

,11 ,Acpess/Work lo.cati~)ll-' 

### .Zone 210 220 Access Door 831 

# ." Manpower' Resources 

## '

. , I!! Manhours 

### 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do thejob Component COMPA01 ITEM H~W P,AATN"



## ,JIi '" 1183387 Consumable CMLA01 ITEM DESCRIPTION

Adhesive tape REFERENCE TO QTY P"ER

### NC CMLMAT.No. DAN269-25 1 (M) ,sEE0 

### 'NCDTES

SEE NQTES

.. 

# + References 

# "' 

# .,,- Fig. A-FBAAA 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 ofSprings on the Strike ofthe Cockpit Door Fig. A-FBBAA Sheet 01 - Principle of Manufacture ofthe Springs

6
3
6 

### (al Remove:

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

Item 1
Item (2) Retain

Retained at removal

5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No.: 00 - Sep 18109 Page: 9 Printed in FRANCE €:IAIRBUS S.A.S. 2007. All rights reserved.

# I ~A340·500/600

SERVICE BULLETIN The springs item 1 can be ordered by a spare purchase order to AIRBUS or manufactured by the operator following the ~ FBBAA Sheet 01. (c) Apply onthe doorthe ~dheSive tape on all surface in contact between the door and the springs item 1.

D. TEST Adhesive tape DAN269-25 1 (M)
(1) Sublask 255169-700-001-001 - Testing

, 

### ~'lWork Z~>nes add'Access Rallelsf; -""",. ,

## "" IwZpne " 

### "I·, '"si'AccesslWoTR1'OCalion 210 220 Access IDoor 831 

# ISkills Manpqwer ResourcesIAIRFRAME
\4 References 

### 1 AircraftMaintenanceManual(AMM) Task52-51-11-820-801 (a) Check that the cockpit Idoor operates properly b~ opening/closing 

### it several times.

If the door is found hard to open (or close), do the adjustment of the door gap (Refer to AMM Task 52-51-11-820-801). E. CLOSE-UP (1) Subtask 255169-942·001-001 - Close-up 

# ': , ,~Wbrk 20n.esand Access Pflnel~ . 

# .'" ,:SZone 

# "", 'I AccesJs!W6rR,tocafion , 

# '" 210 1 

### 220
1---~----------;M~a~n~po::C<w~e~'~R~e~s~o~u=<c~e~S;----;J~----~---- Skills I-A-'R-F-R-A-M-E------ References Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801 (a) Make sure equipment. that the work areas are clean and clear of tools and other items of , (b} Close the passenger/crew door 831 (RefertoAMM Task 52-10-00·410-801). (c) Remove the access platfonn. (d) Restore the systems and the aircraft to normal operating condition. 5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No: 00 - Sep 18/09 Page: 10 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reserved."CONF ALL Z220 

# /

I I 

# I 

# ~~I I Figure A-FBAAA
. Sheet 01 Installation of Springs onthe Strike ofthe Cockpit Door I 5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340·25-5169 REVISION No.: 00 - Sep 18/09 Page: 11 Prillted ill FRANCE © AIRBUS S.A.S. 2D07. All righls reserved.

# $A340.S00/600 SERVICE BULLETIN

dCONF ALL 

## BEFORE

(2)

Figure A-FBAAA ~Sheet 02

Installation 01Springs on the Strike ofthe Cockpit Door 5 DATE: Sep 18/09 SERVICE BULLETIN No.: A340-25-5169 REVISION No.: 00 - Sep 18/09 I Page: 12 Printed in FRANCE Ii)AIRBUS S.A.S. 2007. All rights reserved.

I**CONF ALL

(2} 

# ~A340·500/600 SERVICE BuLLETIN 

# I AFTER

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

COCKPIT DOOR

Figure A-FBAAA'· Sheet 03 Installation of Springs on the Strike ofthe Cockpit Door
5 DATE: Sep 18109 SERVICE BULLETIN No.: A340-25-5169 REVISION No.· 00 -Sep 18/09 Page 13 Printed in FRANCE ©AIRBUS SA$. 2007. All rights reserved_ (

## !$!A340·500/600 SERVICE BUL~ETlN

"CONF ALL PRINCIPLE OF MANUFACTURE 10,,,m 10.394 In) ClAM. 5.82 mm 1922!lin)

20mm (0.787 i,,) R.l0 mm (0.3&4 In) 

# I ,ClAM, ~,~1mm

# I' A"1 10,390In).

# , 

# 1~1J~-

"IOrnm ~~ .I= (0~94In) O~rnl~ --~

__ ' (00121"1


# -- ~ 1
- 

# -1'~~ A::J 1,9mrn'~1 (0.075 In) ."' 

# r-, + ,,-'mm 

# I 100

# -I
-- (O.858Inl 3mm 

# -i- O?7mm· 152. (0.116In) 

# 1'''''"1 ~

•••. 16.6 mm 

# 4)\'",",",
'mm (0,079 In) 50,5m", (2.500 in) 

## A'A

F _SB~\515'U_50M..OI_~2 MATEA(AI. ASNA0322 OR AMS5518OR 1.4310 THICKNESS O,4mm(O.157In) IDENTIFICATION IDENTIFY THE SPRING WITH PART NUMBER 11a30a7 NOTE: NOT SI'ECIFIEO RADIUS: R. 3 mm {0.116 In) 40,2mm (1.5831"1

'mm (0.1971n) 

# ,~ 10.197 In) ~I 

# "o"mm('~- (0.015in) _~_



# "'mm 

# l
(3.267 In) • UNFOLD 10mm '·(0,394 In)

221010 

### ~" A. 0.75 mm 

# .. -1 (0.0~9In) I 

# I -'-' ~O,2 mrn (1.1891")



# , DATE: Scp 18109 Figure A-FBBAA· Sheet 01 Principle 01Manulaclure 01\110 Sprlnlls SERVICE BULLETIN No.: A340·25-S169 REVISION No
.. 00· Sop ISl09 Page: 14 Ptlnl"" In FRANCE 0 AIRBUS SAS, 2001. Anrlgh" le'.No<!,

# ~A340·500/600 I SERVICE BULLETIN Appendix - Elapsed Time Assumption
**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340-25-5169

STEPS MH ET PER

GET ACCESS 0.50 0.50 

# , I

SPRINGS INSTALLATION 0.50 0.50 

# , I I

TEST 0.50 0.50 

# , I I
CLOSE-UP 0.50 0.50 1 

### I I I I I r I
TOTAL MAN HOURS (MJ 0 0.' 1 1.5 2 ELAPSED TIME 20 (HOURS) ELAPSED TIME (El) 2.0

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 

# , DATE: Sep 18/09 SERVICE BULLETIN No.: A34D-25-5169 REVISION No.: 00 - Sep 18109 Page: 1 Printed In FRANCE €:J AIRBUS SAS. 2007, All righls rese/Ved.

### TITLE; 

# ~A~40.500/600 SERVICE BULLETIN I REPORTING SHEET 

### EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR MODIFICATION No.: 200344050120 Please complete the appropriate item (A or B): A - S8 WILL BE embodied I YES/NO (il NO please comment) If YES, aircraft concerned (as per S8 effectivity by default) a~d planned dates (month/year) 01 embodiment: I

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

YES/NO YES/NO If operational documentation is affected (s8,e Paragraph 1.K of this 8B): If information is needed prior to next normal revision or prior to S8 embodirrent. please indicate req~jred service(s}: Either: Modification Operational Impact (MOl), if available Or : Intermediate revision 

# I Important Information: This S8 will only be incorporated in ~our maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in I Updating of maintenance documentation to show pre and post SB data. Updating of maintenance and operatiorl documentation to shoW post SB data after embodiment. If this 58 requires previous or simultaneous accomplishment of oJher SBs, Airbus shall automatically include them in the manual revisions. Refe~ to SIL 00-037 for detailsd information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellante 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX (+33)561 932806 I e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, 58 lists via leiters or fax are also accepted.



### 5 DATE: Sep 18/09 SERVICE BULLETIN No
.. A340-25-5169 REVISION No
.. 00 - Sep 18/09 Page- 1 Printed in FRANyE © AIRBUS SAS. 2007. All rights reserved.

# $A340·500/600

, SERVICE BULLETIN QUALITY PERCEPTION FORM Usethis form to tell us what is your perception 01the 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 thetime you have taken in completing this form. 

# , (Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality ratingofthis 58

- Quality rating ofthe Accomplishment Instructions

- Quality rating of the Illustrations

- Isthis 58 easy to understand? 

### 4 3 4 3 4 3 Y/N 2

2 2
Ifyou have had difficulties in the accomplishment ofthis 58 please quote below the area(s} and give a shorl description 01the issue. I Planning Material Instructions X Effectivity X Kit content I X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identificatlon X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: NameiTitle: Please return thisform to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellante 31707 BLAGNAC CEDEX FRANCE Altn
.SEM4 Service Bulletins Management FAX: (33) 5 51 934251 Orvia your Resident Customer Support Office. 

### Date:

5 DATE: Sep 18/09 REVISION No : 00 -Sep 18/09 Prillted ill FRANCE SERVICE BULLETIN No,: A340-25-5159 

### Page: 1 © "RBU' SAS 2007.'" ,igh" ",,",d