~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) 5 61 934251

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

AlA SYSTEM: 25

TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR

*-CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR I None

MINOR [200344050120 I I I I

NOTE: As per EASA IR 21, a minor change is one thai 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/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 of this 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 (tI8Se)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 OF THE 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

REVISION No.. 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

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel. (33) 5 61 933333

Telex: AIRBU 530526F

Fax: (33) 5 61 934251

ATA SYSTEM: 25

TITLE: EQUIPMENT/FURNISHINGS-COCKPIT - IMPROVE COCKPIT DOOR

MODIFICATION No.: 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

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 shali

not be 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. PLANNING INFORMATION

HCONF ALL

A. EFFECTIVITY

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

intrusion and penetration resistant cockpit door is installed.

(1) Models

340·541 340-542 340-642

(2) Effectivity by MSN

0371037603830391 039404100416-04170426043104360440044504490453

0457 0460 0464 0468 0471 0475 0478 0482 0485 0488 0492 0495 0499 0514 0517

0520 0523 0531 0534 0537 0540 0543 05470557 0560 0563 0566 0569 0572 0575

0577 0580 0583 0586 06010604060606080611061506170619062206240626

0628063006390672 0677 0681068506890694069807020706071007150719

072307270736074007440748075307570761-07680771 0775077907830787

079007940798080408120829083708460848 0870 DB860894 0897 0902 0910

0912091709240929093309530972 09810987 0993 1005 1030 1040

(3) Effectivity by Operator

The OperatorlMSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any fulure changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

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 0566 0569 0580 0583 0762 0763

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 0499 0560 0563

TAM 04450464

THA 062406280677 0681 068906980710071907750953

UAE 0394 0457 0471 0485 0520 0572 0608 0611 06850694

VIA 037103760383039104160449057506150622063907060723

0736 0753 0764 0765 0768 0787 0804

(4) Configuration by MSN

I MSN CONF.IGURATION

0371 0376038303910394041004160417042604310436 001

0440 0445 0449 0453 0457 0460 0464 0468 0471 0475 0478

04820485048804920495049905140517052005230531

0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572 ,

05750577 0580 0583 058p 060106040606060806110615

061706190622062406260628063006390672 0677 0681 ,

06850689069406980702070607100715071907230727

0736074007440748075307570761 0762076307640765

0766 0767 0768 0771 0775 0779 0783 0787 0790 0794 0798

08040812082908370846084808700886089408970902

0910 0912 0917 0924 0929 0933 0953 0972 0981 0987 0993

100510301040

(5) Configuration definition

*·CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this 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 door frame.

(3) Advantages I

Accomplishment of this 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

E. COMPLIANCE

(1) Install the Springs on the Strike of th,e Cockpit 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.
G. MANPOWER

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 Strike of t~e Cockpit Door. 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

ThIS Service Bulletin is the subject of aniAIRBUS monitored retrofit campaign.

Component COMPA01

(2) Price and Availability

No AIRBUS kit will 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

For o~dering 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 01 this 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 no charge tor the operator.

The man·hours indicated in this Service Bulletin will remain at the 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. LIST OF MATERIALS· OPERATOR SUPPLIED

,

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIRTION '

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 IN THE REFERENCED PROCEDURES,

I

ALWAYS OBEY THE PRECAUTIONS THAT FOLlOV! TO ,{[EP

ELECTRiCAL WIRING iN A SATiSFACTORY COh;DiTiOt\j RiCALLY

l\NO :vH::,CHANICALLYSERViCE.ABLE) WHE~~ YOU DD Mi\INT:J,J/\\C[~

WORK. REF'AIRS OR 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 OTHER

CONTA~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) Subtask 255169-910-001-001 - Standard Practices

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

NON SPECIFIC

!- __'-?0&:-;R:ete~ndes

Aircraft Maintenance (vlanual(AMM) Task 20-21-11-911-801

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) Clean the work area with.

I

Solvent General 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

I

NON SPECIFIC

Write in the applicable air~raft records that 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;laAcceq ~~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 Task 52-10-00-010-801

(a) Make sure that the! aircraft is electrically grounded (Refer to AMM Task

12·34-24-860-802) .

(b) Put access platform in position

(c) Open the passenger/crew door 831 (ReIer to 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 of the Cockpit Door.

""Work Zones and A~ess panels

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

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 the job

Component COMPA01

ITEM H~W P,AAT N"

,JIi '"

1183387

Consumable CMLA01

ITEM DESCRIPTION

Adhesive tape

REFERENCE TO QTY P"ERNC

CMLMAT.No.

DAN269-25 1 (M)

,sEE0

'NCDTES

SEE

NQTES

.. + References

"' .,,-

Fig. A-FBAAA 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

Fig. A-FBBAA Sheet 01 - Principle of Manufacture of the

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 on the door the ~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

,

~'lWorkZ~>nesadd'Access Rallelsf; -""",. , ""

IwZpne " "I·, '"si'AccesslWoTR1'OCalion

210

220 Access IDoor 831

ISkills

Manpqwer ResourcesIAIRFRAME

\4 References 1

Aircraft MaintenanceManual (AMM) Task 52-51-11-820-801

(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.es and 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 (Refer to AMM 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 on the Strike of the 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 of the 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 of the 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

10,390 In).

,

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

O?7mm· 152. (0.116 3mmIn)-i- 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) _~_

(3.267

"'mm

In)

l•

UNFOLD

10mm

'·(0,394 In)

221010

~

"

A. 0.75 mm

.. -1 (0.0~9In)

I

I

-'-'

~O,2mrn

(1.1891")

, DATE: Scp 18109

Figure A-FBBAA· Sheet 01

Principle 01Manulaclure 01\110Sprlnlls

SERVICE BULLETIN No.: A340·25-S169

REVISION No.. 00· Sop ISl09 Page: 14

Ptlnl"" In FRANCE 0 AIRBUS SAS, 2001. An rlgh" 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

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Please return this completed sheet to:

AIRBUS

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e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

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REVISION No .. 00 - Sep 18/09 Page- 1

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SERVICE BULLETIN

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Date:

5 DATE: Sep 18/09

REVISION No : 00 - Sep 18/09

Prillted ill FRANCE

SERVICE BULLETIN No,: A340-25-5159

Page: 1

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