SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel: (33) 5 61 933333 Telex: AIABU 530526F Fax: (33) 561 934251 This summary is for information only and is not approved for modification ofthe aircraft. ATA SYSTEM: 25 

### TITLE: EQUIPMENT 

### I FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT "CONF ALL MODIFICATIONS MODIFICATION CLA~SIFICATION MAJOR INone MINOR 113545023270 

## I I I I

As per EASA IA 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness ofthe product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES The A310 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 doorframe. I Accomplishment ofthis Service Bulletin wiil improve the cockpit door reliability GENERAL EVALUATION 

### EVALUATION IT ABLE COMPLIANCE RECOMMENDED CANCELS iNSPECTION SB 

### NO POTENTIAL AD 

### NO A/8 OPERATION AFFECTED 

### NO RELIABILITY AFFECTED 

### YES PAX COMFORT AFFECTED 

### NO COST SAVING 

### NO ETOPS 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 AlC (USD) Component COMPA01 1 See S8 Springs


### 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No.: 00 - Sep 21109 Page: 1 Printed in FRANCE ., AIRBUS SAS. 2007. All rights reserved.

# $A310 SERVICE BULLETIN SUMMARY EFFECTIVITY This Service Bulletin is applicable to this (these) operator{s) : 34W 52X 58X 99Y AlL AFG AIB AIC BAF BBC BLE CFC CSA DAH DEC DGA F21 FOX GAF HFY 12L IRA IRM lYE JAB JAV KAC KTC KYV KZU MGL MWA PIA QAF Rn RJA ROT RZO SBI SGX SUO TSC UZB WHT CONCURRENT REQUIREMENTS None REFERENCES I REPERCUSSIONS TFU None OEB None AOT None SIL 

### None LINE MAINTENANCE AFFECTED No LIFE LIMIT 

### None OTHER 

### None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO 1 OBRM NO MANPOWER Task- 252206-831-801-00"1: Modification TOTAL MANHOURS 12.00 ELAPSED TIME (HOURS) 1200 APPENDICES Appendix - Elapsed Time Assumption



### 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No.: 00 - Sep 21109 Page: 2 Printed in FRANCE eAIRBUS SAS. 2007. All rights reserved., 

# (!!;,A310

, SERVICE BUULETIN SUMMARY
"CONF ALL

Figure A-FSAAA - Sheet 01 I IFR138 

### lE..B.11

5 DATE: Sep 21/09 SERVICE BULLETIN No,. A310"25-2206 REVISION No :00 - Sep 21/09 Page: 3 Printed in FRANCE © AIRBUS SAS. 2007. All rights reserved

# I~A310 SERVICE BULLETIN SUMMARY
*~CONFALL

SPRING TO BEADDED

Figure A-FSAAA - Sheet 02 ,
5 DATE: Sep 21/09 SERVICE BULLETIN No
.. A310-25-2206 REVISION No. 00 - Sep 21/09 Page: 4 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.SERVICE BULLETIN AIRBUS CUSTOMERSERVICESDIRECTORATE 1 Rond PointMauriceBellante 31707 BLAGNACCEDEX FRANCE Tel: (33)561 933333 Telex: AIRBU530526F Fax: (33)561 934251 ATA SYSTEM:25 

### TITLE: EQUIPMENT/ FURNISHINGS" COCKPIT" DOOR MODULE

IMPROVEMENT : MODIFICATION No: 13545023270 This document contains AIRBUS PROPRIETARY IN~ORMATION and shall at all times remain the property ofAIRBUS; no Intellectualproperty right or licence is granted byAIRBUS in connection with any information contained in it. It is delivered on the !expresscondition that said document and the information containedin itshall betreated as confidential,shall notbe usedfor any purposeotherthan thatforwhich itis herebydelivered. Itshall notbedisclosed inwholeorin parttothird partiesandshall not be duplicated in any manner (exceptforthe purposes ofperformingthe tasks described hereunder and provided that any recipient of such document sh~1Icomply with the conditions herein). without AIRBUS priorwrittenconsent. I 1. PLANNING INFORMATION HCONF ALL A. EFFECTIVITY NOTE: This SeNice bulletin is onlyI applicable to aircraft on which the modified

intrusionand penetration resistantcockpitdoorisinstalled. (1) Models 310-203 310-324 310-204V 310-222

310-324F 310-325 31O-2

# 42V 310-304 310·304T 310-308 A310·308FA310-324F 310-322 (2) Effectivityby MSN 0291 0293030903200338 035703670370037203750378-03790386 0389-0390 039203990406-04070410041304160418-04190421-0422 04250427-0431 0434 0436-043704390441 04440446-044904680472-047304750481-04890491-0492 0494-049905030519-05200522-05240526-05270531 05370541054505470549 05620564-05650567,05680571 0573-057405760585-05880590-0591 0594-0595 05970599"0600062006220624063606380640064206440646-06540656 0658 0660-0661 06630665066706690671-0672 067406760678068006820686-0687 06890691 06970700 070207040706

5 DATE:Sep 21/09 SERVICE BULLETIN No,:A310-25-2206 REVISION No
.00-Sep21/09 Page: 1 Printed in FRANCE © AIRBUS SAS. 2007. All rights reserved.I

# ~A310 SERVICE BULLETIN (3) Effectivity byOperator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance wit~the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this lisl unless the Service Bulletin is revised for another reason. I 

### OP~I\JOR 'it , 

### C!I\ 

## iAMsI'l: C' 

### 34W 0399 

### 52X 0410 

### 58X 0431 

### 99Y 0489 

### A1L 0648 

### AFG 04960497 

### AIB 0686 

### AIC 0392 0406 0407 0413 0428 0429 0654 0665 0669 0680 

### BAF 036703?? 

### BBC 0594070b 

### BLE 0650 

## I CFC 0425 044

### J 0444 0446 0482 

### CSA 0672067~ 

### DAH 0291 0293 

### DEC 0697 I 

### DGA 0418 042~ 0422 

### F21 0309 

### FOX 0378 0439 0449 0492 0549 0638 

### GAF 0434 0484 0498 0499 0503 0522 0523 

### HFY 04950565 

### 12L 06400642 

### IRA 0338 0370 0375 0379 0389 0390 0436 0671 

### IRM 0488 0537 0564 0586 

### lYE 0568 070~ 0704 

### JAB 0320 041~ 

### JAV 0357 048j1 

### KAC 0647 0649 0663 

### KTC 0524 056,70620 

### KYV 0386 

### KZU 0622064'6 

### MGL 0526 

### MWA 0652 

### PIA 0473 058,50587 0590 0653 0656 0660 0676 0678 0682 0687 0689

0691 

### QAF 0667 

### Rn 0591 

### RJA 0416049,1 0531 

### ROT 06360644 

### RZQ 0571 06240651 0661 

### SSI 0427043004680475048604870520 5 DATE: Sep 21/09 SERVICE BULLETINNo.: A310-25-2206 REVISION No
.. 00 - Sep 21/09 Page: 2 Printed in FRANCE © AIRBUS S.A.S. 2007, All rights reserved,

# ~A310 SERVICE BU~LETIN 'OPERl'.,T0Rl 

# '" ':C 

## """C 

# l' ~"MSN" ""'::'~"~lI1If: 

### q; 

# " SGX 05190562 

## I SUD 

### 0437 

## I TSC 044704720483048505270541054505470588059505970599

06000658 I UZB 057405760706 

## I WHT 0448 0494 0573 

## I (4) Configuration by MSN ",~
.M?0Nl~'::' 0291 0293 0309 0320 0338 0357 0367 0370 0372 0375 0378 03790386038903900392039904060407041004130416 0418041904210422042504270428042904300431 0434 04360437043904410444 044604470448044904680472 047304750481 04820483048404850486048704880489 0491 0492049404950496049704980499050305190520 05220523052405260527 053105370541 054505470549 05620564056505670568 0571 05730574057605850586 0587058805900591 0594 059505970599 0600 06200622 

# ~~;~ 6~~~ 6~;~ ~~:~ 6~~~ ~~~: ~~:~ 

# t~:~ 6~:~ 6~:; 6~~~ 06690671 067206740676067806800682068606870689 0691 069707000702 0704 0706 I (5) Configurationdefinition CO'NFIGtJRATfOr;..l"' 001

~~n~i~.Fo~~1iS

valid forall theaircraftgivbn intheeffectivityofthis Service Bulletinasa standardconfiguration. (6) Material Effectivity 

### :"@Ar~RiALi: ComponentCOMPAOl ConsumableCMLA01 

### B. CONCURRENT REQUIREMENTS None 

### C. REASON (1) History ,·0l;p,Y,PERA:/&: SE;.sJ,:!OTES 1 As required

TheA310 aircraft in-serviceexperience hasshownthaI cockpitdoor installation mustbe improved. (2) Objective/Action This Service Bulletin recommends to modify the cockpit door installation by adding springsand adhesivetapesonthedoorframe. 5 DATE: Sep 21/09 SERVICE BULLETIN No.:A310-25-2206 REVISION No:00
. Sep21/09 Page:3 Printed in FRANCE © AIRBUS S.A.S. 2007. All righls reserved

# I~A310 SERVICE BULLETIN (3) Advantages Accomplishment 01this Service Bulletin will improve the cockpit door reliability. (4) Operational/Maintenance 

### cdnsequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary 10 : Task 252206-831-801-001: Modi\ication (1) Install the Springs on the Strike of the Cockpit Door. 

### E. COMPLIANCE (1) Classification RECOMMENDED (2) Accomplishment Timescale Accomplishment 01 this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL Approved under EASA Design Organisation Approval No, EASA21J.031. If an aircraft listed in the effeJlivitY has a modification or repair embodied thaI is not of AIRBUS origin. and which affects the content of thiS Service Bulletin, the operator is responsible for obtaining approvi11 by Its airworthiness authority for any adaptation necessary before incorporation of the 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 to suit operator's circumstances. The estimates do not include the time to prepare, plan or inspect the work: Manufacture and procurement 01 parts and tools, drying times for paints, sealants. etc., and general administration work are also not Included, It~,_p 

# ,,",,"'. 0~J:,{sk:¥252206.~83!S8Q 1"OO~i Modificatlp~< 

# .'" " Get Access 0.50 On Aircraft Install the Springs on the Strike of t,heCockpit Door, 0.50 Tests 0,,50 Close-Up 0,50 TOTAL MANHOURS 2.00
5 DATE. Sep 21/09 SERVICE BULLETIN No.' A310-25-2206 REVISION No
. 00
. Sep 21/09 Page: 4 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# ~A310 SERVICE BUJLETIN 

# I

lime assumption, refer 10 Appendix " o(;ljficatioil 2.00 For detail concerning the Elapsed Time Assumption NOTE: Task -252206.;S31-8(} ELAPSED TIME (HOURS)

H. WEIGHTAND BALANCE NotChanged I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Maintenance Manual (AMM) 20-21-12 24-00-00 52-1000 52-51-'1 Consumable Materia! Ust (CML) Elee. Std. Practices Manual (ESPM) 20-55-00 Structural Repair Manual (SRM) 51-40~20 K. PUBLICATION AFFECTED IlIlustrated Parts Catalog (IPC) L. INTERCHANGEABILITYIMIXABILITY Not Applicable M. SPARES None

5 DATE: Sep 21/09 SERVICE BULLETIN No."A310·2S-2206 REVISION No : 00 - Sep 21/09 Page: 5 Printed in FRANCE ©AIRBUS S.A.S. 2007. Po.!1 rights reserved.I

# ~A310 SERVICE BULLETIN

This ptge Intentionally Left Blank

------------



### 5 DATE: Sep 21/09 REVISION No: 00 -Sep 21/09 SERVICE BULLETIN No.: A310-25"2206 Page: 6 Printed in FRANCE ©AIRBUS SAS.2007. All rights reserved.

# ~A310 SERVICE BUJLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAilABILITY (1) Procurement Addresses This Service Bulletin isthe subject ofan AIRBUS monitored retrofit campaign. Component COMPAQ1

(2) Priceand Availability No AIRBUS kit will be provided. Customers with aircraft shown in the effecti~ity of this Service Bulletin should send a pur6hase order to AIRBUS. Quote the numbJr of this Service Bulletin. The address ;" I Airbus: Spares Support and Services Weg~eimjaeger 150 D-223~5Hamburg Germany For ordering by internet http://spares .airbus .com For orpering 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 a spares purchase order to AIRBUS. B. INDUSTRY SUPPORT INFORMATION For the organisation of this retrofit, operators' are kindly requested to contact AIRBUS retrofit management department. I AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Be[lonte 31707 BLAGNACCEDEX France Tel (33)567190622 E-mail: monitored.retrofit@airbus.com Fax: (33)561 932745 Parts are at no charge for the operator. The man-hours indicated in this Service Bulletin will remain at the operators' cost. 

# c. LIST OFCOMPONENTS No Kit

5 DATE: Sep 21/09 SERVICE BULLETIN No: A310-25-2206 REVISION No : 00 - Sep 21/09 Page: 7 Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.

## D. (1) Consumable Malerials Consumable CMLA01
Solvent General Purpose Adhesive tape (2) Components Component COMPA01 

### REF~.R~j'19):'TtI·CMLf MALNQ>".~' "" 11-026 DAN269-25 As required 

### '1M)

(3) Equipment 

### None E. PARTSTO BE RE-IDENTIFIEDBYOPERATOR 

### None F. TOOLING 

### None

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No.: 00
. Sep 21/09 Page: 8 Printed In FRANCE © AIRBUS SAS. 2007. All rights reserved.

# ~A310 SERVICE BUJLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 252206-831-801-001 --Modification WARNING: MAKE SURE THAT YOU OBEY AlLL THE WARNINGS AND AL.L THE CAUTIONS

iNCLUDED IN THE REFERENCE9 PROCEDURES. Cf\JTD_.f~.. !;;,LWAYS OBEY rHE PRECAUTiONS THAT FOLLOW 1'0 l(EEF'

LLLCHi:CAL VV:RNG IN A S.fTlSFACTORY C01<0ITI0\) LU~CFliC::ALLY ANI) ~.I1EChAN,CALL Y SERVICEABLE)_ WHEN YO:J DO Mi\i0iTEN!\f\iCE WORK. R::PM4S (-JRMODIFICATIONS, ALWAVS K_:_P L, ::::CH~CA. \V<R1f\,G CmA"'ONE-NTS AND THE WOJr<. Ie; 1:::6

. AS 81 -A\ N" ass ,;LE TO 00 THIS. PUT PRor~CT10N. sue" 

### ,1l.S: PLAS]I;:; SHEETING C
.. DII'S '::lC, AS NECESSARY ON WiRING AND GOMPONENTS ~~~~;~~~T~~OVE ALLSHiVINGS' UNWANTEDMArERIALAND OTHER THESE PRECAUTiONS WILL qEGREASE THE RISK OF COf\iTAM!:".JArON AND D/\\lAGE TO THE ELSGTHfCAL ';ViH NG !NSTAlLf~rON IN CASE OF CONT.l\MINATIO~J ~E.FER TO E$PM 20 550D Task Associated 

### Data



### A. GENERAL (1) Subtask 252206-910-001-001 _~ManpbwEf~>" ,'it1' '_",,',,',',', I

I 2.00 I 2.00 I

- Standard Practices

I



### SEE N015S Skills I NON SPECIFIC I 

# I·
. ~;ll~l!iiJJili~~'§~ssa_lDeJ)j!jI.l\il!l 

# *. I I 

# ,c:f1.EPpREI1~q<i -, GM,Ef'MAifyNo:' Solvent General Purpose 11

### ·Of!6 I ,f.~EHere'rfc- Aircraft Maintenance Manual (AMM) 20-2~-12 

### 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310"25·2206 REVISION No.: 00 - Sep 21/09 Page: 9 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reservedI

# I~A310 rRVICE BULLETIN RefexelJ:CJ}s,~,,_ t!' Consumable Material List (CML) Struclural Repair Manual (SRM) I

# I (a) For the specification!o!the Material Lisl (CML). 

# I (b) Clean the work area W1ith
. SolventGeneral 11"-026 Purpose 51-40-20 material numbers (Mat. No.). refer to Consumable

As required (c) For the removal and Installation of fasteners (Refer to SRM 51-40-20). (d) To torque tighten the standard threaded fasteners (Reier to AMM 20-21 12). I (2) Subtask 252206-839-001-001 - Administrative I 

## "IaiI' ef

## Re§ Skills 

## I Write in the applicable airbraft records that you have done all the work given in this Service Bulletin. B. PREPARATION



## I I Kjfan,power Res"9

## ur't,e,S".,%-' 

## I AIRFRAME I 'Zone 210 

### 220 (1) Sublask 252206·941-001-001 - Job Set-up



# I ';t~Work:'l.Qne_saDg'iA.cE:e_ss -·panels"
4" 

# ,f:Yj' 

### Ace.ess'CWQrkfCfCfltlon

Skills '5H _Reta:f,e,nc~s Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301



# I 52-10-00, Page Block 001 (a) Make sure that the aJcraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). 

# I (b) Put access platform in position (cl Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001).

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No
.. 00 - Sep 21/09 Page: 10 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# ~A31°
SERVICE BUI.JLETIN 

### C. PROCEDURE

0,50 1 0.50 AIRFRAME (1) Subtask 252206-831-001-001 - Install the Springs on the Strike of the Cockpit Door. I 

## d'/'f.,c,

## ess1Ra11eJ ' --lk{;



### .. '~"~:At~ce,



## .s1WOrk'iocarroJj I Door 8311I ;Manpm:ver";Ff' ,"'" ',.,:y: I

I I I I 

### '~aWi;}~:1

# (;l~Ces~sajy,·~~,difft~t~~>~,< I I I 

## €ll;\i;@MIii, 

# KE~~6R\fr~
, ~)if~

# <_co ,>".44 3 I Spring I I 

## fJ,t'f':' EN~~

\,O? 9t;~,_~"R,@'C

~ .. ]:",No,.,- 

## ,:~iji:, DAN269-25 1 (M) I



### ~ ~efe.reJiGes>", f:
.

### r;!:' "":-,-,

Sheet 01 - Installation of Springs on the Strike 01the Cockpit Door Sheet 02 - Installation of Springs on the Strike of the Cockpit Door Sheet 03 - Installation of Springs on the Strike of the Cockpit Door Sheet 01 - PrinCiple of Manufacture of the Springs Fig. A·FBBAA Fig. A-FBAAA Manhours Minimum number of person Subtask elapsed time Skills

6
3

6 (a) Remove.

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

Item 1

Ilem (2) Retain

Retained at removal NOTE: 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310~25~2206 REVISION No.' 00 - Sep 21/09 Page: 11 Printed in FRANCE <V AIRBU~ SAS, 2007. All rights reserved.I

# I~A310 SERVICE BULLETIN The Jin9S item t can be ocdeced by a space pucehase oedec to AIRBUS or manufactured by the operator following the 

## Bg. AFBBAA'Sheet 01. (e) Apply on the door the ~dheSive tape on all surface in contact between the door and the springs ilem 1. 

# I Adhesive tape DAN269-25 1 (M) D. TEST

AIRFRAME 

# I I Door 831 

### I fyian

## powJ~ffij_e~9l!rce&? 

## I I (1) Sublask 252206-700-001-001 -Testing I <:~V;;tork~bnes,anij



### Access ·pa.:nel5:

- Access"'iwot-j(;;Jocatlb'r(4:

Skills
Aircraft Maintenance Manual (AM~) 52-51-11, Page Block 501 (a) Check that the 

### COCkPit

# ldoor operates properly by opening/closing 

### itseveral times.

Ifthe door is fOU~dhard to open (orclose), dothe adjustment of the door gap (Refer to AMM 52-51·11, Page Block 501). E. CLOSE-UP

AIRFRAME - Close-up 

### It)

Skills
Aircraft Maintenance Manual (AMM) ~eeJ~fl ,~;~,' w>--'C_- 52-10·00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the passengeriCrew door 831 (Refer to AMM 52-10-00, Page Block 001).



# I (c) Remove the access platform. (d) Restore the systems Ld the aircraft to normal operating condition. 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No
.. 00 - Sep 21/09 Page: 12 Printed in FRANCE © AIRBUS SAS_ 2007 All rights reserved_

# ~A310 SERVICE BULLETIN

"CONF ALL



# o I IFR13s lEB.1l

5 DATE: Sep 21109 Figure A-FBAAA - Sheet 01 Installation of Springs on the Strike ofthe Cockpit Door SERVICE BULLETIN No.: A310-25-2206 REVISION No.: 00 - Sep21/09 Page: 13 Printed in FRANCE ©AIRBUS SAS. 2007, All rights reserved.

# I~A310 SERVICE BULLETIN

*""CONFALL 

## BEFORE

I 

# ~@] I Figure A· FBAAA - Sheet 02 installation of Sprihgs on the Strike of the Cockpit Door (2)

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No.: 00 - Sep 21/09 Page: 14 Pril1led in FRANCE © AIRBUS SAS. 2007. All rights reserved.

# 'SiA310 SERVICE BULLETIN

"CONF ALL 

## AFTER

(2)

APPLY ON THE DOOR THE ADHESIVE TAPE DAN 269-25

ON ALL SURFACE IN CONTACT BETWEEN THE DOOR AND THE SPRINGS.

COCKPIT DOOR 

# IFWD) A-A

5 DATE: Sep 21109 Figure A-FBAAA - Sheet 03 Installation of Springs on the Strike ofthe Cockpit Door SERVICE BULLETIN No.: A310-25-2206 REVISION No.: 00 -Sep 21109 Page: 15 Printed in FRANCE C AIRBUS S.A.S. 2Q07.All rights reserved.

## $A310 SERVICE BULLETIN

··CONF ALL PRINCIPLE OF MANUFACTURE



# A:J DIAM, 5.02 nHl' (0.229 In)

20mm (0.787 In) 

# Ai

~- 

# ~;==-T-=~-+--

03mm
--- (0.394 ~i1) 10:012 In) 

# """'====-

# =='~-~~-,

I

53.Smm 12.500 in) ,.gmm II 

## IQ.0751nlfr (:,~ mill 

# r-,:lr'"h""O' I 100·(
-- - 21.amm 37.7 mrn (0.85<1in) (l.4e4ln) 152

_ 3mrn I

~ 10.118;01---....-1..
154 .--.... 10,6 mm

10.654 In)

'mm (0,079 In) A-A 

# 'Mmm('

# t:k lO.Ol!>;n) _~_



### ~

# -.' _R.O,75mm

(O,029in) 

# , 30.2 mm --- -- . (1.189 In) ~ - - 

# --FT="0- --~- I 

# L 22mm I' 25mm ~--~ Smm 4D2mm (G.as6Onl ,(Q.984'lnl ~I0.1S7inl (1.583 In) 

# [- -+---l - I ,;:::, -----------
'" I 83,5mm 5 mrn (3,267Inl 

## I 10,m7 in) UNFOLD • Figure A-F88AA - Sheel Q1 Principle of Manulaclure of the Springs MATERIAL ASNA3322 OR AMS55180R 1.4310 THICKNESS 0.4 rnm (0.157 inl tDEN"TlFICIITION IDENTIFY THE SPRING WITH PART NUMBER 11833B7
NOTE: NOT SrECIFIED RADIUS: R~ 3 mm (O,118In)
6_Sa_2'i?2,",_'_BaAA_01_"'

5 DATE:Sep 21109 REVISION No.: 00· Sap 21109 P,I"'eo illFRANGE SERVICE BULLETIN No.: A310-25-2208 Page: 1& @All'teuS S.A.S. 2001. Allrighi' f.so",.d,

# ~A310 SERVICE BUJLETIN Appendix - Elapsed 

### Time Assumption
"CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No A310-25-2206

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 I I 

### I

CLOSE-UP 0.50 0.50 1 I 

### I

0 05 I 1.5 2 ELAPSED TIME TOTAL MANHOURS (MH) 2.0 (HOURS) ELAPSED TIME (El) 2.0

MH: MANHOURS ET: ELAPSED TIME PER: NUMBER OF PERSONS NOTE: THIS CHART IS ONLY pt.. PROPOSAL OPERATORS MAY DEljERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM,

Figure A-FAAAA l Sheet 01 Appendix - Elapsed Time Assumption
5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISIONNo,:00· Sep21/09 Page: 1 Printed in FRANCE ©AIRBUS SAS. 2007, All rights reserved.

### TITLE: 

# ~A310 SERVICE BULLETIN REPORTING SHEET 

### EQUIPMENT/ FURNIS~INGS •COCKPIT - DOOR MODULE IMPROVEMENT I MODIFICATION No.: 13545023270 Please complete the appropriate item (A on B): A - S8 WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SBleffeclivily by default) and planned dates (month/year) of embodiment:

B - S8 HAS BEEN embodied on aircraft: Operator comments;
From Airline: NameiTitle: Signature: Dale: Ifoperational documentation is affected (s~e Paragraph 1.K of this S8): If information is needed prior to next normal revision or prior to S8 embodl(nent, please indicate required service(s}: Either: Modification Operational Impact (MOl), if available YES/NO Or : Intermediate revision 

# I YES/NO Important Information: This 58 will onl~ be incorporated in your maintenance and operational documentation il this sheet is returned to ,Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in

# I

- Updating 01 maintenance documentation to show pre and post 58 data. Updating 01 maintenance and operatiohal documentation to show post 58 data alter embodiment. II this SB requires previous or simultaneJus accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Referl to SiL 00-037 for detailed 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 Documeltation Services FAX: (+33)561 932806 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, S8 lists via letters or fax are klso accepted.

5 DATE: Sep 21/09 SERVICE BULLETIN No,: A310~25-2206 REVISION No
.. 00 - Sep 21/09 Page' 1 Printed In FRANCE ©AIRBUS S.A.S. 2007. All rights rBsBIVBd(Please ~ateon a scale of 1 to 4, with 4 being the highest score)

-Quality rating ofthis S8

-Quality rating ofthe Accomplishment Instructions

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- Isthis S8 easy to understand? 

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Ifyou have had difficulties in the accomplishment ofthis S8 please quote below the area(s} and give a short description ofthe issue. Planning Material Instructions X Effectivity X Kitcontent X Preparation X Reason X Listof 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: Namerritle: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellante 31707 BLAGNAC CEDEX FRANCE Attn :SEM4 Service Bulletins Management FAX: (33) 5 61 934251 Orvia your Resident Customer Support Office. Date:

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206 REVISION No,: 00 - Sep 21/09 Page: 1 Printed in FRANCE © AIRBUS SAS. 2007. All rights reserved. I