TITLE:

$A300r600

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rand Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel (33) 5 61 933333

Telex: AIRBU 530526F

Fax: (33) 5 61 934251 I

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

AlA SYSTEM: 25

EQUIPMENT I FURNISHINGS - COCKPIT· DOOR MODULE

IMPROVEMENT

*~CONF ALL

MODIFICATIONS

MODIFICATION CLftjSSIJ=JCATION'

MAJOR INone

MINOR 1 13545D23270 , I

As per EASA IR 21, a minor Chang~ is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness 01 the product. All other Cianges are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The A300-600 aircraft in-service experience has show1n that cockpit door closing mechanism must be

improved, I

This Service Bulletin recommends to modify the cockpit door closing mechanism by adding spring

steels on the door frame. I

Accomplishment of this Service Bulletin will improve the cockpit door closing system.

GENERAL EVALUATION I

~VALUATIONI TABLE

COMPLIANCE RECOMMENDED CJj\NCELS INSPECTION S8 NO

POTENTIAL AD NO Ale OPERATION AFFECTED NO

RELIABILITY AFFECTED YES P4J( COMFORT AFFECTED NO

COST SAVING NO EtOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFqRMATION TABLE

MATERIAL SET aTY PER PRICE PER , MAIN PARTS

Ale Ale (UpD)

Component COMPA01 1 See SB, Springs

5 DATE: Sep 21/09 SERVICE BULLETIN No_: A300-25-6218

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

Printed in FRANCE © AIRBUS S,AS. 2007. All rights reserved.
~A300·600

SERVICE BULLETIN

SUMMARY

EFFECTIVlTV

This Service Bulletin is applicable to this (these) operator(s) :

AAl ABO AHK AMU CES CSN DLH F21 FDX G8E IRA IRM JAL

KAC KAL LAA MON MSR MXU OHY QIR SUO TAR THA UZ8

CONCURRENT REQUIREMENTS

None

REFERENCES I REPERCUSSIONS

TFU None

OEB Non~

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO I

HARD NO I

SOFT NO

OBRM NO

MANPOWER

Task 256218-831-801-001: Modification

TOTAL MANHOURS 2,00

ELAPSED TIME (HOURS) 2.00

APPENDICES

Appendix" Elapsed Time Assumption

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

REVISION No_ 00 - Sep 21/09 Page: 2

Printed in FRANCE © AIRBUS SAS, 2007. All rights reserved.
~A300r600

SER~18~~~k~ETIN

··CONF ALL

Figure A-FSAAA Sheet 01

5 DATE: Sep 21/09 SERVICE BULLETIN No,; A300-25-6218

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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
~A300·600

SERVICE BULLETIN

SUMMARY

HCONF ALL

SPRING TO

BE ADDED

Figure A-FSAAA - Sheet 02

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

REVISION No_.00 - Sep 21/09 Page. 4

Printed in FRANCE ©AIRBUS SAS. 2007. All rights reserved.
~A300·600

SERVICE BULLETIN

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

AlA SYSTEM: 25

TITLE: EQUIPMENT I FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT

MODIFICATION No.: 13545023270

This document contains AIRBUS PROPRIETARY INfOAMATION and shall al all limes remain the

prpperty 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 10Ihird parties and shall

not be duplicated in any manner (except for the purposes of perionning 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

··CONF ALL

A. EFFECTIVITY

(1) .Models

84-601

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

intrusion and penetration resistant cockpit door is installed.

84-603 84-605R 84-620 84-622 B4-622R F4-605R

(2) Effectivity by MSN

028402940301030703120317032103360341 03480351 0368038003980401

0405040804110414041704230459-04610463-0466 0469-0470 0474 0505-0518

0521 05250529-05300532053605400543 0546 0553-0561 0563056605690572

05750577 0579 0581·0582 0584 0601-0613 0615-0619 062106230625-06330635

063706390641 064306450657065906620664066606680670067306750677

0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711

07130715071707190721-072507270729-07340737 0739-07410743-0744

0746-0747 0749..()750 0753-0754 0756 0762·0764 0767 0770 0773 0775 0782-0788

0793 0797 0836·0838 0855-0860 0870-0871 0873-0878

5 DATE:Sep 21/09 SERVICE BULLETINNo.: A3na·25-6218

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

Printed in FRANCE @AIRBUS S.A.S. 2007. All rights reserved.
~A300·600

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

<7IlJ'~~1f~fl" ',Z v~, ,~,'. "C' ," M~N1ii' T/'Zli

~

C.j)

AAL 0423 0459 0460 0461 0463 0466 0469 0470 0474 0506 0507 0508

05090510051105120513051405150516 0517 0606 0610 0612

0615061906260639064306450675

ABO 0529 0557

AHK 0855 0856 0857 0858 0859 0860 0870 0871

AMU 0677 0743

CES 0521 052505320707072507320741 074607540763

CSN 0733 073!.l.0739 0750 0756 0762

OLH 03800401 040504080618062307010773

F21 0284 029~ 0301 0307031203170321 0336034103480351

FOX 0417 053p 0536 0543 0555 0559 0572 0575 0579 058106110613

062506300633065706590664066806880709071307150793

08730874087508760877 0878

G8E 0465

IRA 0632 0696 0723 0727

IRM 0411 0414 0546 0553 0608

JAL 0602 06H 0621 06370641 06700679068307030711 07240729

0730073707400753077007830797083608370838

KAC 0673 069A- 0699 0719 0721

KAL 0582060.906270631 0662068506920731

LAA 0601 06lf)

MON 0540 055:60604 0605

MSR 0561 060:'7

MXU 07670788

OHY 0584 06d3 0744 0747 0749 0764

QTR 0554056'0

SUO 06660775

TAR 0505 0558 0563

THA 0368039804640518056605690577 0628 0629 0635 0681 0705

0782 0784 0785 0786 0787

UZB 07170722

5 DATE: Sep 21/09 SERVICE BULLETINNo.: A300"25-6218

REVISIONNo_:00 - Sep 21/09 Page: 2

Printed in FRANCE © AIRBUS SAS. 2007. All rights reserved.
~A300~600

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

02840294030103070312031703210336034103480351 001

03680380039804010405040804110414041704230459

04600461 046304640465046604690470047405050506

0507050805090510 05110512 0513 0514 0515 0516 0517

0518 0521 0525 0529 0530 0532 0536 0540 0543 0546 0553

05540555 0556 0557 0558 0559 0560 0561 0563 0566 0569

0572 0575 0577 0579 0581 0582 0564 0601 0602 0603 0604

0605 0606 0607 0608 0609 06100611 0612061306150616

0617 0618 0618 0621 0623 06250626 0627 0628 0629 0630

0631 0632 0633 0635 0637 0639 0641 0643 0645 0657 0659

0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683

0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709

0711 07130715 0717 0719 072107220723072407250727

0729 0730 0731 0732 0733 0734 0737 0739 0740 0741 0743

0744 0746 07470749075007530754 0756 0762 0763 0764

0767 0770 0773 0775 0782 0783 0784 0785 0786 0787 0788

0793 0797 0836 0837 0838 0855 0856 0857 0858 0859 0860

08700871 0873 0874 0875 0876 0877 0878

(5) Configuration definition

··CQNF 001

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

standard configuration.

{6} Material Effectivity

MATERIAL ""'j:,_, .

.

, QTY PER A/C SEE NOTES1#L _

Component COMPA01 1

Consumable CMLA01 As required

CURRENT REQUIREMENTS

SON

(1 ) History

None

B. CON

c. REA

The A300-600 aircraft In-serVice

mechanism must be improved.

experience has shown that cockpit door closing

I

(2) Objective/Action

This Service Bulletin recommends to modify the cockpit door closing mechanism by

adding spring steels on the door frame.

(3) Advantages

Accomplishment of this Service Bulletin will improve the cockpit door closing system.

5 DATE: Sep 21109 SERVICE BULLETIN No.: A300-25-6218

REVISION No.: 00 - Sep 21109 Page: 3

Prinled in FRANCE C AIRBUS S.A.S. 2007. All rights reserved.
~A300·600

SERVICE BULLETIN

(4) Operational/MainlenancecJ,seq"",ces

None

D. DESCRIPTION

To accomplish this Service Bulletin it is neCessary to .

Task 256218-831-801-001: Modification

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

E. COMPLIANCE

(1) Classification

RECOMMENDED

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilitits are available.

F.

G.

APPROVAL

Approved under EASA Design O(Qanisation Approval No. EASA 21J.031.

II an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approvkl by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

MANPOWER I

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 inspe.ct the work. Manufacture and procurement of parts

and tools, drying times lor paints, sealants, etc., and general administration work are also not

included.

,e , Ta§k'25§~i8-831-8U1';'001: MQdificati9r1

Get Access 0.50

On Aircraft

Install the Springs on the Strike of the Cockpit Door. 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

5

NOTE:

DATE: Sep 21109

For detail concerning the elapsed time assumption, refer to Appendix -

Elapsed Time Assumption.

SERVICE BULLETIN No.: A300-25-6218

REVISION No.: 00 - Sep 21/09 Page: 4

Prinled in FRANCE © AIRBUS SAS. 2007. All rights reserved.
$A3001S00

SERVICE BU~LETIN

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICALLOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM)

I

20-21·12 24-00-00 52-10-00

52"51-11

Consumable Material List (CML) I

Elee, Std. Practices Manual (ESPM) I 2055 00

Structural Repair Manual (SRM) I 51-40-20

5

K. PUBLICATION AFFECTED

1IIIustrated Parts Catalog (IPC)

L. ~TERCHANGEAB1LlTY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

REVISION No . 00 - Sep 21/09 Page: 5

Printed in FRANCE © AIRBUS SAS. 2007. All rights reserved.

I
~A300·600

SIERVICE BULLETIN

This Page Intentionally Left Blank

5 DATE: Sep 21/09

REVISION No.: 00· Sep 21/09

SERVICE BULLETIN No_.A300·25·6218

Page 6

Printl'!d In FRANCE © AIRBUS SA.S. 2007, All rights rleserved.
$A300·600

SERVICE BULLETIN

2. MATERIALINFORMATION

UCONF ALL

A. MATERIAL - PRICE AND AVAilABILITY

(1) Procurement Addresses

This Service Bulletin is the subject 01 an AIRBUS 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

numbbr of this Service Bulletin. The address

is' I

Airbus Spares Support and Services , Weg beim jaeger 150

D-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 relrofit

management department.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BlAGNAC CEDEX

France

Tel: (33) 5 67 19 06 22

E-mail: monitored_retrofit@airbus_com

Fax: (33) 5 61 932745

Parts are al 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,: A300·25-621a

REVISION No: 00 - Sep 21/09 Page: 7

Printed in FRANCE e AIRBUS S.A.S. 2007. All rights reserved,
~A300·600

SERVICE BULLETIN

D. LIST OF MATERIALS· OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLAOl

ITEM DESCRIPTION IREFERENCE TO,CML QTY PER Ale SEE

, MAT."No. NOTES

Solvent General Purpose 11-026 As required

Adhesive tape DAN269-25 '1M}

(2) Components

Component COMPAQ1

iTEM NE';fPART N' QTY (UM) iEYWORD ITEM' Gt!DPART N' ' ,

INT SEE' "

Pi ' ,

/: -'1" NClTES

1 1183387 3 Spring

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

5 DATE: Sep 21/09 SERVICE BULLETIN No_: A300-25-6218

REVISION No : 00 - Sep 21/09 Page: 8

Printed in FRANCE It>AIRBUS SAS. 2007. All rights reserved.
~A30016o0

SERVICE BUJLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 256218-831-801-001 - Modification

~'

"

Zone'

I

TOTAL MANHOURS

ELAPSED TIME (HOURS)

~~~~g~~~NT~:; ~~FUE~~~6t~~~~~~~~~~.GS AND ALL THE CAUTIONS

ALWA~'S OBEY TH OHFJ"AUT!ONS THAT FOLLOW Te KEEP

ELECTRiCALWJRj\i(, IN A ::;~TISrACTORY CO!\lDITION (ELECTRiCAllY

AND MECHANICALLY 8C:JiVICE,A8LEi \;VHEN YOU 00 MtdNF.i\jA\GE

;f"ORK ,1. RE"PAIRS' ~ OR MO'uIF'I;""""!C'~;~ ''','"''II, A~J< 'A'L,.", 'MAV','d K,-'r:P "_~_ .,;::

..,_,_,\.' !:::"]'PI"A: \.'. ~

\'\'fiRil"'G ._,.' i "

COMPONENTS AND THE VV01K /,HCA P,S CLEAN :\8 POSS TO DO

'THIS:

PUT PROTECTION, SUCH A~ PLASTiC SHEETING, CLOTHS. ETC- 1\'8

NECESSARY ON WiRiNG AND (COMPONENTS

, I

ci~~~~~~N:TPIOENM,'OM,[ All Sf!r"\GS, UNWANTED MATER!AL AGiD OTd'R

THESE PRECAUTIONS WilL tpECREASE THE RISK OF CONTJ1J~~,:rJf\TIO\l

AND DNAAGE TO THE ElECTRICAI_ WIRING INSTALLL\TION

Task ASSOCiale~ND::S!C Of OONTt,M,N!1i!ON rFCRTO FSP,", 2D~55~Q!)

WARNING:

CAUTION,.

A. GENERAL

(1)

Consumable CMLA01

!tE;M~ ~~ 'O:ESct ",','," ,

NON SPECIFIC

5 DATE: Sep 21/09 SERVICE BULLETIN No.' A300-25-6218

REVISION No : 00 - Sep 21/09 Page: 9

Printed in FRANCE © AIRBUS S.A.S. 2007, All rights reserved,

,
~A300·600

SERVICE BULLETIN

r F.letere6ce~t

Consumable Malerial List (CML)

Structural Repair Manual (SRM)

(a) For the specification 0Il f the material numbers (Mat. No.), refer to Consumable

Material List (CML).

,

(b) Clean the work area with:

Solvent General

Purpose

11c026 As required

(e) For the removal and installation of fasteners (Refer to SRM 51-40-20).

(d) To torque tighten the standard threaded fasteners (Refer to AMM 20-21 12).

Skills

(2) Subtask 256218-839-001-001 - Administrative

i

M;anpgVll,8n F\?~YJce~:<,%:1

I NON SPECIFIC

Write in the applicable aircraft records that you

Service Bulletin,

have done all the work given in this

B. PREPARATION

AIRFRAME

a;;'Ac:~'}>Parf~r

_AQcess~rK (oea

(1) Subtask 256218-941-001-001 . Job Set-up

I

Skills

"p RefeJenceSt

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 I 52-10-00, Page Block 001

I

(a) Make sure that the aitcraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put access platform in position

(c) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001).

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

REVISION No,: 00 - Sep 21/09 Page: 10

Prillted ill FRANCE © AIRBUS S,A.S, 2007. All rights reserved,
~A30016o0

SERVICE BUJlETIN

C. PROCEDURE

0.50

1

0.50

AIRFRAME

- ._~:..,".~

Sheet 01 . Installation of Springs on the

Strike of the Cockpit Door

Sheet 02 - Installation 01 Springs on the

Strike of the Cockpil Door

Sheet 03 - Installation of Springs on the

Strikb of the Cockpit Door

Sheet 01 - Principle of Manufacture of the

Springs

Access

Zone'

210

220

(1) Subtask 256218-831-001-001 - Install the Springs on the Strike of the CoCkpit Door.

I

orl{.Zones-§'h'a &, ,esS"Patlels

:if "fjccij ,stWlii n:,

I

Door 8311

I

Fig. A-FBBAA

Manhours

Minimum number of person

Subtask elapsed time

Skills

Component COMPAOl

:T~M ~.~:ltN

1183387

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.: A300-25-6218

REVISION No : 00 . Sep 21/09 Page: 11

Printed in FRANCE © AIRBUS SAS. 2007, All rights reserved.
(c)

$A300·600

I

SERVICE BULLETIN

The j;ngs ;rem 1 can be ordered by a spare purchase order

to AIRBUS or manufactured by the operator following the ~

FBBAA Sheet 01.

Apply on the door the AI dhesive tape on all surface in contact between the door and

the springs item 1. .

Adhesive tape DAN269-25 1 (M)

D. TEST

(1) Subtask 256218-700-001-001 - Testing

&J.k .~ h-e-l <

210

220 Access

Skills

I Door 831

I

,l~JI!!!'c~s~

I AIRFRAME

I

tal Check thaI the COCkPitldoor operates properly by opening/closing il several times.

- If the door is founC! hard to open (or close), do the adjustment of the door gap

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

E. CLOSE-UP

(1) Sublask 256218-942-001-001 - Close-up

I

"'tone -~n(fAC~_~s'-;pa_lJels:

""'J\c'ee~sP.Ndrklcieatrbn.' "'0 •

Ef$~~1;i~{e

Aircraft Maintenance Manual (AM~) 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 paSSenger/crew door 831

(cl Remove the access platform.

(Refer to AMM 52-10-00, Page Block 001)_

(d) Restore the systems and the aircraft to normal operating condition.

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

REVISION No.: 00 - Sep 21/09 Page: 12

Printed in FRANCE © AIRBUS $AS. 2007. All rights reserved.
~A300·600

SERVICE BULLETIN

*"CONF ALL

I IFR13B

lE£ill.

<7)

Figure A-FBAAA - Sheet 01

Installation of Springs on the Strike of the Cockpit Door ,

5 DATE: Sap 21109 SERVICE BULLETIN No : A300-25-6218

REVISION No.: 00 - Sap 21109 Page: 13

Printed in FRANCE e AIRBUS SAS. 2007_ All rights reserved.
~A300·600

SERVICE BULLETIN

*'CONF 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.: A300-25-6218

REVISION No: 00 - Sep 21/09 Page: 14

Pnnted in FRANCE © AIRBUS SAS. 2007. All rights reserved.
~A300i600

SERVICE BULLETIN

**CONF ALL

(2)

APPLY ON THE DOOR THE

ADHESIVE TAPE DAN 269-25

ON ALL SURFACE IN

CONTACT 8ETWEEN 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

SERVICE BULLETIN No.: A30a·25-6218

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

Prlrlted In FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

I
!$;A300·600

SERVICE BULLETIN

"CONF ALL

PRINCIPLE OF MANUFACTURE

• mm

«(),D79 in)

10mm

{Q.S94in)

'OQ'

1.9m".,

(0,075 in)

37,7mm ?o',8mm

1

1 (0.858in) k"jf' ,"',;,~",--.1

154 '6.6mm

(0.664 in)

\ '

A. 'Omm

(0,39'1 in) AI

DIAM. 9,91 ",rn

(0,350 in)

I-'"mm -i (-i2E\

I (0,9i5In) ~- ¥-

0.3

~~--+~ mrn

{O.304:n) {O.OI~ln)

~~~~~~~-~-l '---:1

20 rnrn

(0,787 In)

DIAM. 5,82 ",rn

{Q.229 i,,)

63.5mm

(2.500 In)

A-A

83.5mm

(3,287 In)

UNFOLD

---:---=-T-TTHICKNESS

0.4 mm(0.157In)

IllENTlflCATION

IDENTIFY THE SPRING WITH PART

NUMBER 1183387

O_SS_25021a_5_H3AA_~I_"2

MATERIAL

ASNA332:200

AMS5S'S OR

1.4310

NOTE:

NOT SPECIFIED RADIUS: R~ 3 mm {O,lla in)

(0,'97In)

5 rnm ~0.2rnrn -~#,I'r"'

'mm

, ,

RO",,""(" ~

{O.OI6Inl _~~ _

I

: 25mrn

I(0,964 In)

~2mm

{O.66S in)

10mm

(0.394 In)

~

'

, R O.l5mm _.. -1 {O.029in)

I

L

30.2 mrn

(1.189 I,,)

, DATE: Sep 21/09

Figure A-F8BAA· Sheet 01

Principle or ManuJaclure ot the Springs

SERVICE BULLETIN No.. A300·25·6218

REVISION NQ.: 00· Sep 2,/09 Page: ,S

P,i'''e~ In FRANCE " AIRBUS S.A,S. 2007, All ';(11)1,•• , ••.• ed.
$A3001600

SERVICE BUJLETIN

Appendix - Elapsed Time Assumption

NOTE: THIS CHART IS ONLY /!I PROPOSAL.

OPERATORS MAY DEtERMINE THAT ANOTHER WAY

MH: MAN TO DO THE WORK IS ORE SUITABLE FOR THEM, HOURS

ET: ELAPSED TIME

PER: NUMBER OF PERSONS

**CONF ALL

ELAPSED TIME ASSUMPTIONS S RVICE BULLETIN No. A300-25-6218

STEPS MH ET PER

GET ACCESS 0.50 0,50 I

I

SPRINGS INSTALLATION 0.50 0,50 I I I

TEST 0.50 0.50 1 I I

CLOSE-UP 0.50 050 1 I I

I I I I

0 05 1 1.5 2

ELAPSED TIME

TOTAL MANHOURS (MH) 20 (HOURS)

ELAPSED TIME (El) 20

,

Figure A-FAAAA f Sheet 01

Appendix - Elapsed Time Assumption

5 DATE Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

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

Printed in FRANCE © AIRBUS SA5. 2007. All rights reserved.
TITLE:

~:Jl300·600

J,ERVICE BULLETIN

EQUIPMENT I FURNISJ:::T~N:OS;:::T _ DOOR MODULE

IMPROVEMENT

MODIFICATION No_: 13545023270

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Or . Intermediate revision

Important Information: This SB will only be incorporated in your maintenance and operational

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the next feasible revision, this will result in I

- Updating of maintenance documentation to show pre and post S8 data.

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If this S8 requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

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Please relurn this completed sheet to:

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5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218

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

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~A300·600

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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Y I N

2

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2

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Planning Material Instructions

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Date:

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25·6218

REVISION No,: 00 - Sep 21109 Page: 1

Printed in FRANCE 0 AIRBUS SAS. 2007. All rights reserved.