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) 5 61 934251

This summary is for information only and is not approved for modification of the aircraft.

ATA SYSTEM: 25

TITLE: EQUIPMENT I FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT

"CONF ALL

MODIFICATIONS

MODIFICATION CLA~SIFICATION

MAJOR I None

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 of the 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 door frame. I

Accomplishment of this Service Bulletin wiil improve the cockpit door reliability

GENERAL EVALUATION

EVALUATION ITABLE

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.
,

(!!;,A31, 0

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

*~CONF ALL

SPRING TO

BE ADDED

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

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellante

31707 BLAGNAC CEDEX

FRANCE

Tel: (33) 5 61 93 33 33

Telex: AIRBU 530526F

Fax: (33) 5 61 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 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

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document sh~1Icomply with the conditions herein). without

AIRBUS prior written consent. I

1. PLANNING INFORMATION

HCONF ALL

A. EFFECTIVITY

NOTE: This SeNice bulletin is onlyI applicable to aircraft on which the modified

intrusion and penetration resistant cockpit door is installed.

(1) Models

310-203

310-324

310-204V 310-222

310-324F 310-325

31O-242V 310-304 310·304T 310-308

A310·308FA310-324F

310-322

(2) Effectivity by MSN

0291 0293 0309 0320 0338 0357 0367 0370 0372 0375 0378-0379 0386 0389-0390

039203990406-04070410041304160418-04190421-0422 0425 0427-0431 0434

0436-043704390441 04440446-044904680472-047304750481-04890491-0492

0494-049905030519-05200522-05240526-05270531 05370541054505470549

05620564-05650567,05680571 0573-057405760585-05880590-0591 0594-0595

0597 0599"0600 0620 0622 0624 0636 0638 0640 0642 0644 0646-0654 0656 0658

0660-0661 06630665066706690671-0672 0674 0676 0678 0680 0682 0686-0687

0689 0691 0697 0700 0702 0704 0706

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

~A310

SERVICE BULLETIN

(3) Effectivity by Operator

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 0672 067~

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 056,7 0620

KYV 0386

KZU 0622064'6

MGL 0526

MWA 0652

PIA 0473 058,5 0587 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 0446 0447 0448 0449 0468 0472

047304750481 04820483048404850486048704880489

0491 0492049404950496049704980499050305190520

05220523052405260527 053105370541 054505470549

05620564056505670568 0571 05730574057605850586

0587 0588 0590 0591 0594 0595 0597 0599 0600 0620 0622

~~;~6~~~6~;~~~:~6~~~~~~: ~~:~t~:~6~:~6~:;6~~~

06690671 067206740676067806800682068606870689

0691 0697 0700 0702 0704 0706 I

(5) Configuration definition

CO'NFIGtJRATfOr;..l"'

001

~~n~i~.Fo~~1iSvalid for all the aircraft givbn in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

:"@Ar~RiALi:

Component COMPAOl

Consumable CMLA01

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

,·0l;p,Y,PERA:/&: SE;.sJ,:!OTES

1

As required

The A310 aircraft in-service experience has shown thaI 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 door frame.

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A310-25-2206

REVISION No : 00 . Sep 21/09 Page: 3

Printed in FRANCE © AIRBUS S.A.S. 2007. All righls reserved
I~A310

SERVICE BULLETIN

(3) Advantages

Accomplishment 01 this 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, EASA 21J.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,

I t~,_p ,,",,"'. 0~J:,{sk:¥252206.~83!S8Q 1"OO~iModificatlp~< .'" "

Get Access 0.50

On Aircraft

Install the Springs on the Strike of t,he Cockpit 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. WEIGHT AND BALANCE

Not Changed

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 is the subject of an AIRBUS monitored retrofit campaign.

Component COMPAQ1

(2) Price and 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 ~eim jaeger 150

D-223~5 Hamburg

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 BLAGNAC CEDEX

France

Tel (33) 5 67190622

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 OF COMPONENTS

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·CM Lf

MAL NQ>".~' " "

11-026

DAN269-25

As required

'1M)

(3) Equipment

None

E. PARTSTO BE RE-IDENTIFIED BY OPERATOR

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 (-JR MODIFICATIONS, 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 ALL SHiVINGS' UNWANTEDMArERIAL AND 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 reserved
I

I~A310

rRVICE BULLETIN

t!' RefexelJ:CJ}s,~,,_

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.

Solvent General 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"9ur'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'CWQrk fCfCfltlon

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 8311

I

;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 <VAIRBU~ 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,anijAccess ·pa.:nel5:

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

Skills

Aircraft Maintenance Manual (AM~) 52-51-11, Page Block 501

(a) Check that the COCkPitl door operates properly by opening/closing it several times.

If the door is fOU~dhard to open (or close), do the adjustment of the door gap

(Refer to AMM 52-51·11, Page Block 501).

E. CLOSE-UP

AIRFRAME

It) - Close-up

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 of the Cockpit Door

SERVICE BULLETIN No.: A310-25-2206

REVISION No.: 00 - Sep 21/09 Page: 13

Printed in FRANCE © AIRBUS SAS. 2007, All rights reserved.
I~A310

SERVICE BULLETIN

*""CONF ALL

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 of the 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<1 in)

(l.4e4ln) 152 _ 3mrn I

~

10.118;01---....-1..

154 .--.... 10,6 mm

10.654 In)

'mm

(0,079 In)

A-A

'Mmm(' lO.Ol!>;n) _~_ t:k

~

-

.' _R.O,75mm

(O,029in)

,

30.2 mm --- -- .

(1.189 In) ~ - - --FT="0- --~- I

L

22mm I' 25mm ~--~ Smm 4D2mm

(G.

as6On

l ,(Q.984'ln

l

~I0.1S7inl (1.583In)

[- -+---l -

I ,;:::, -----------

'" I

83,5 mm 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 ill FRANGE

SERVICE BULLETIN No.: A310-25-2208

Page: 1&

@All'teuS S.A.S. 2001. All righi' 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

REVISION No,: 00· Sep 21/09 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:

If operational 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) 5 61 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 of this S8

- Quality rating of the Accomplishment Instructions

- Quality rating oi the Illustrations

- Is this S8 easy to understand?

4 3

4 3

4 3

VIN

2

2

2

If you have had difficulties in the accomplishment of this S8 please quote below the area(s} and give a

short description of 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:

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

Or via 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