~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 of this Service Bulletin will improve the cockpit door reliability.

GENERAL EVALUATION

I EVALUATION if ABLE

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 OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD Nol

SOFT Nol

OBRM Nol

MANPOWER

Task 2543~6·~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 e AIRBUS 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 - Sep 21/09 Page: 3

Printed in FRANCE © AIRBUS SAS. 2007. All rights reserved.
**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) 5 61 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

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

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

n01be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein). without

AIRBUS prior written consent.

1. PLANNINGINFORMATION

"CONF ALL

A. EFFECTIVITY

This Service bulletin is only applicable to aircraft on which the modified

intrusion and penetration resistant cockpit door is installed.

(1) Models

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

(2) Effectivity by MSN

0002-000900110013-00150018-00290031-0035 0038-0041 0043-00440046-0049

0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085 0088-0091

0093-0094009701010103-01040114-011501170123 0125·0126 0128-0129 0131

0133-013701390141-01420145-01470149-01520154 0156-01610163-0164

0166-01700173-01760178-018001820185-01870190 0192-0194 0196-0197 0199

0201-020202040207-020802100212-02180220-0221 02250227-02280233

0235-0~37 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270

0273-0274027802800282029202970302030403070310 0318-0319 03210325

032703290331-03320335034703520354-035503590363 0367 0373-0374

0377-0379038103850387039003950399040204060411 0413-04150424

0429-04300433-0435043804420446-04470450045904670470 0474 0483 0528

0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646

0651 0668 0793 0800 0835 0844 0921 0938 0955

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) Effectivity by Operator

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 01 an aircraft from one operator to another will not be reflecled in

this list unless the Service Bulletin is revised for another 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 02B2 0554

HFY 0117

IBE 0005 OO~B0125 0134 0145 0146 0170 0193 0197 0217 0221 0302

031803290332037803870414045904740483

KAC 0089 OO~O0101 0104

LAN 0167 03$9 0363 0429 0442

LHT 0274 I

M3R 0061 I

MAU 0076 00Q4 0152 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 BULLETIN No.: A340-25-4326

REVISION No.: 00 - Sep 21IU9 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 '0192 0193 0194 0196 0197

01990201 020202040207020802100212021302140215

02160217021802200221 022502270228023302350236

0237 0239 0242 0243 0245 0246 0252 0257 0260 0263 0264

02680270027302740278028002820292029703020304

030703100318031903210325032703290331 03320335

0347035203540355035903630367037303740377 0378

0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413

0414 0415 0424 0429 0430 0433 0434 0435 0438 0442 0446

0447045004590467047004740483052805380541 0544

0545 0546 055'40556 0559 0561 0562 0582 0585 0590 0598

064306460651 066807930800083508440921 09380955

(5) Configuration definition

"CONFIGJj XA110~1

001

dCONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

fOIATERIi':(w " ","'ilil,"t, •,;",,"~".~' .-' "'" ". ,'" '+'N;~. • ,Q;T.l!!f'E~?Ii!(Dli? SSfu~~$i'%'+

Component COMPAOl 1

Consumable C'MLAOl As required

B. CONCURRENT REQUIREMENTS

None

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326

REVISION No.: 00 - Sep 21/09 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 on the door frame.

(3) Advantages I

Accomplishment of this serce Bulletin will improve the cockpit door reliability.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 254326-831·801-001: Modification

(1) Install the Springs on the Strike of the Cockpit Door.

E. COMPLIANCE

(1) Classification

RECOMMENDED

F. APPROVAL

(2) Accomplishment Timescal,

Accomplishment of this ~ervice Bulletin is

where manpower and facilities are available.

I

recommended at the earliest opportunity

Approved under EASA Design Organisation Approval No. EASA 21J.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

responsible for obtaining approval by its airworthiness authority lor any adaptation necessary

before incorporation of the Service Bulletin.

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25A326

REVISION No.: 00 - Sep 21109 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 10 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 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:ojftPJi)10

Gel Access 0.50

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 rigl1ts reserved,
~A340

SERVICE BULLETIN

This Page Intentionally Left Blank

5 DATE: Sep 21/09

REVISION No.: 00 - Sep 21/09

Printed in FRAiCE

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) Price and Availa'bility

No AIRBUS kit will be provided.

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purqhase order to AIRBUS. Quote the

number 01 this 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

For ordering 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.

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 for the operator.

The man-hours indic1ted in this 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.,LlY

AND MECHANICALLY SERV]CEA3LEi WHEN YOU 00 MAINTENANCE

WORK. REPA!RS OR MODIF1CATJONS. ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AMEA AS 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

I NON 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 - Sep 21109 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

(a) For the specification of the material numberk

Malerial List (CML).

w\< I ~i~"" ~*~)pJ:<.lere'lce_S-<N: .~''''- j't11\-

Consumable Material List (CMl)

Structural Repair Manual (SRM)

(b) Clean the work area with:

~~~~~:~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 applicable aircraft records that 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 12-34-24-8

1

60-802

I Task 52-10-00 0110-801

(a) Make sure that thJ aircraft is electricalI) grounded (Refer to AMM Task

12-34-24-860-802). I

(b) Put access platform i1 position I

(e) Open the passenger/crew door 831 (Refer to 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 of the 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 of the 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

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

10 AIRBUS or manufactured by the operator following the ~

FBB4 Sheet 01, I

(e) Apply on the door the :Adhesive tape on all surface in contact between the door and

the springs item 1. I

Adhesive tape DAN269~25 1 (M)

D. TEST

(1) Sublask 254326-700-001-001 . Testing

Access Door 831

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 Maintenance Manual (AM~) Task 52-51-11-8?0-801

{al Check that the COCkPiJdoor operates properly dy opening/closing it several times.

If the door is fOU~d hard 10 open (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.fResJ2Ur~._

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

Figure A-FBAAA - Sheet 01

Installation of Springs on the Strike of the Cockpit Door

SERVICE BULLETIN No.: A340-25-4326

REVISION No.: 00 - Sep 21109 Page: 13

Prinled In FRANCE e AtRBUS S.A.S. 2007. All rights reserved.
I

I~A340

SERVICE BULLETIN

HCONF ALL

BEFORE

(2)

Figure A-FBAAA - Sheet 02

Installation of Springs on the Strike of the 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

REVISION No : 00 - Sep 21/09 Page: 15

Printed in FRANCE 1) AIRBUS SAS. 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

37'r-:100'( --~f 21.81"11"1

.7mm? (0,858in)

1144841101 152~I...J (o31~8~nl--l

154 le8mm

(0654 In)

,.

R. 10 n""

,10.394 In)

,DIAM. 9.91 mm I

(0.390 In),

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) _~_

p.2871nl "'-'mm-=- •• I

UNFOLD

-----1-1---

, 25m01 !(0,98'1101

101"11"1

{O.394 In)

~

.,

, A. 0.75 mm

- - -) (0,02910)

1

30.2 mm

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'.d InFRANCE 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.
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TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IM1ROVE COCKPIT DOOR

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5 DATE: Sep 21/09 SERVICE BULLETIN No.: A340-25-4326

REVISION No: 00 - Sep 21/09 Page: 1

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SERVICE BULLETIN

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5 DATE. Sep 21/09 SERVICE BULLETIN No.: A340-25-4326

REVISION No.: 00 - Sep 21/09 Page: 1

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