### TITLE: 

# $A300

# r 600 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 isapplicable tothis (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 OFTHE 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 Printedin FRANCE ©AIRBUS SAS. 2007. All rightsreserved.

# ~A300·600 SERVICE BULLETIN AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Point Maurice Bellante 31707 BLAGNAC CEDEX FRANCE Tel: (33)561 933333 Telex: AIRBU 530526F Fax: (33)561 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 betreated asconfidential, shall not be used for any purpose otherthan thatforwhichit is herebydelivered. Itshall notbedisclosed inwhole orin part10Ihird partiesandshall notbeduplicated in any manner(exceptforthe purposesof perionning thetasks described hereunder and provided that any recipient of such document shall comply with the conditions herein). without AIRBUSpriorwrittenconsent 1. PLANNING INFORMATION 

### ··CONF ALL A. EFFECTIVITY
(1) .Models 84-601 This Service bulletin is only applicable to aircraft on which the modified

intrusionandpenetrationresistantcockpitdoorisinstalled.
84-603 84-605R 84-620 84-622 B4-622R F4-605R (2) Effectivityby 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..()7500753-0754 0756 0762·0764 0767 0770 0773 0775 0782-0788 0793 0797 0836·0838 0855-0860 0870-0871 0873-0878

5 DATE:Sep 21/09 SERVICEBULLETIN No.: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 onlyand iscorrect atthe time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer ofan aircraft from one operatorto 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 06060610 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 0284029~ 0301 0307031203170321 0336034103480351 

### FOX 0417 053p0536 0543 0555 0559 0572 0575 0579 058106110613

062506300633065706590664066806880709071307150793 08730874087508760877 0878 

### G8E 0465 

### IRA 06320696 0723 0727 

### IRM 0411 04140546 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 07440747 0749 0764 

### QTR 0554056'0 

### SUO 06660775 

### TAR 0505 0558 0563 

### THA 0368039804640518056605690577 0628 0629 0635 0681 0705

07820784 0785 0786 0787 

### UZB 07170722

5 DATE: Sep 21/09 SERVICEBULLETIN No.: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 05130514051505160517 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 06270628 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 07340737 0739 0740 0741 0743 0744 0746 07470749075007530754 0756 0762 0763 0764 0767 0770 07730775 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 isvalid for allthe aircraft given inthe effectivity ofthis Service Bulletin asa standard configuration. {6} Material Effectivity MATERIAL 

## ""'j:,_, . 

# . , QTY PERA/C SEE NOTES1#L

_ Component COMPA01 1 Consumable CMLA01 As required CURRENT REQUIREMENTS


### SON History (1) 

### 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 onthe doorframe. (3) Advantages Accomplishment ofthis 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/Mainlenance cJ,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 areavailable. F.



### G. APPROVAL Approved under EASA Design O(QanisationApproval No. EASA21J.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 ofthe Service Bulletin. MANPOWER 

## I The manpower estimates given 'inthis 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 orinspe.ctthe 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§~i 8-831-8U1';'001:MQdificati9r1 GetAccess 0.50 OnAircraft Installthe Springs onthe Strike ofthe 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 -

ElapsedTime Assumption. SERVICE BULLETIN No.:A300-25-6218 REVISION No.: 00 -Sep21/09 Page: 4 Prinled in FRANCE ©AIRBUS SAS. 2007. All rights reserved.

# $A300

# 1S00 SERVICE BU~LETIN
H. WEIGHT AND BALANCE Not Changed I. ELECTRICALLOADDATA 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· Sep21/09 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 NoAIRBUS kitwill be provided. Customers with aircraft shown in the effectivity ofthis 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 Forordering byfax: +49.40.50.76.25.90

Parts required to accomplish this Service Bulletin can be manufactured by the operator following the Fig.A-FBBAA orordered bya spares purchase order toAIRBUS. B. INDUSTRY SUPPORT INFORMATION Forthe 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) 567 190622 E-mail: monitored_retrofit@airbus_com Fax: (33)5 61 932745 Partsare al nocharge forthe operator. The man-hours indicated inthis Service Bulletin will remain atthe operators' cost. 

## c. LIST OFCOMPONENTS 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. LISTOF 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. PARTSTO BE RE-IDENTIFIED BYOPERATOR 

### 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 ANDALLTHE CAUTIONS ALWA~'S OBEY TH OHFJ"AUT!ONS THAT FOLLOW Te KEEP ELECTRiCALWJRj\i(, IN A ::;~TISrACTORYCO!\lDITION(ELECTRiCAllY AND MECHANICALLY 8C:JiVICE,A8LEi \;VHEN YOU 00 MtdNF.i\jA\GE ;f"ORK RE"PAIRS'OR MO'uIF'I;""""!C'~;~ 'A' 'MAV',' K,-'r:P ;:: !:::"]'PI"A: \'\'fiRil"'G ,1. ~ 

## ''','"''II, A~J< L,.", d "_~_ ., .. ,_,_,\.' \.'. ~ ._,.' 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

# rFCR TO 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 0Ilf the material numbers (Mat. No.), refer to Consumable Material List (CML).

, (b) Cleantheworkareawith: 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 (RefertoAMM 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 Block301



# I 52-10-00, Page Block 001 

## I (a) Make sure that the aitcraft is electrically grounded (Refer to AMM 24-00-00, Page Block301). (b) Putaccess platform in position (c) Openthe passenger/crew door831 (RefertoAMM 52-10-00, Page Block001).

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 01Springs onthe Strike of the Cockpil Door Sheet 03 - Installation of Springs on the Strikb ofthe Cockpit Door Sheet 01 - Principle of Manufacture ofthe 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 8311I

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 onthe doorthe AI dhesivetape on all surface incontact between thedoor 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 Door831 

### I 

# ,l~JI!!!'c~s~ I AIRFRAME 

### I
tal CheckthaI the 

### COCkPitldoor operates properly byopening/closing il several times.

- If the door is founC! hard to open (or close), do the adjustment of the door gap (RefertoAMM 52[51-11, Page Block501). E. CLOSE-UP (1) Sublask 256218-942-001-001 - Close-up



# I "'tone -~n(f

AC~_~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 Printedin FRANCE ©AIRBUS $AS. 2007.All rights reserved.

# ~A300·600 SERVICE BULLETIN
*"CONFALL



### I IFR13B 

### lE£ill.



## <7)

Figure A-FBAAA -Sheet 01 Installation ofSprings onthe Strike ofthe Cockpit Door



# , 5 DATE: Sap 21109 SERVICE BULLETIN No:A300-25-6218 REVISION No.: 00 -Sap 21109 Page: 13 Printed in FRANCE 

### eAIRBUS SAS. 2007_All rights reserved.

# ~A300·600 SERVICE BULLETIN
*'CONF ALL 

## BEFORE

(2)

FigureA-FBAAA -Sheet 02 Installation ofSprings ontheStrike ofthe 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

ONALL SURFACE IN CONTACT 8ETWEEN THE DOOR AND THE SPRINGS.

COCKPIT DOOR



## ~ A-A

5 DATE: Sep 21/09 Figure A·FBAAA - Sheet 03 Installation ofSprings onthe Strike ofthe 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 OFMANUFACTURE

• mm «(),D79in) 10mm {Q.S94in)
'OQ' 1.9m"., (0,075 in)

37,7mm ?o',8mm 11 (0.858 in) 

# 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) ~- 

# ¥- ~~--+~ 0.3mrn {O.304:n) {O.OI~ln) 

# ~-~-l 

# ~~~~~~ '---:1 20rnrn (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) 5rnm ~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~ InFRANCE " 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 TO DO THE WORK IS ORE SUITABLE FOR THEM, MH: MAN 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 REVISIONNo:00-Sep21/09 Page: 1 Printed in FRANCE ©AIRBUS SA5. 2007. All rights reserved.

### TITLE: 

# ~:Jl300·600 J,ERVICE BULLETIN 

### EQUIPMENT IFURNISJ:::T~N:OS;:::T

_DOOR MODULE IMPROVEMENT MODIFICATION No_: 13545023270 Please complete the appropriate item (Aor B): A - S8 WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per S8 effectivity by default) and planned dates (month/year) of embodiment:
B -S8 HAS BEEN embodied on aircraft: Operator comments: From Airline: NamelTitle: Signature: Date:

YES/NO YES/NO Ifoperational documentation is affected (see Paragraph 1,K of this SB), If Information is needed prior to next normal revision or prior to S8 embodi~enl, please indicate required service(s}' Either: Modification Operational Impact (M<DI),if available , Or
. Intermediate revision Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to !Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in

# I

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

- Updating of maintenance and operatiohal documentation to show post S8 data alter embodiment. If this S8 requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Rele~ to SIL 00-037 !or detailed information. Please relurn this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point MaUrice Bellante 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documen~ation Services FAX: (+33) 5 61 932806 

# I e-mail: sb.reporting@airbus.com or via your Resident Customer Support Oflice. Alternatively, S8 lists via ietters or fax are also accepted.

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-6218 REVISION No.. 00 - Sep 21/09 Page: 1 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reserved.

# ~A300·600 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception 01 the quality of this Service Bulletin. The reported data thaI you provide uswill be used to analyse areas ofdifficulties and 10take corrective action tofurther improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rale on a scale of 1 to 4, with 4 being the highest score)

- Quality rating 01 this S8

- Quality rating 01 the Accomplishment Instructions

. Quality rating of the Illustrations

- Is this S8 easy 10understand? 

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Ifyou have had difficulties in the accomplishment of this S8 please quote below the area(s) and give a short description ofthe issue. I Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X Ust 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: NamefTitle: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rand Pain! 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.: A300-25·6218 REVISION No,: 00 - Sep 21109 Page: 1 Printedin FRANCE 0 AIRBUSSAS. 2007.All rightsreserved.