# ~A300 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

This summary is for information only and is not approved for modification of the aircraft. AlA SYSTEM: 25 

### TITLE: EQUIPMENT I FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT UCONF ALL MODIFICATIONS 

## I MODIFICATION CLASSIFICATION MAJOR None MINOR 113545023270 

## I I 

## I I NOTE: 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. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES The A300 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 EVALUATION TABLE COMPLIANCE RECOMMENDED CANCELS INSPECTION S8 

### NO POTENTIAL AD 

### NO NC 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 INFO!3:MATION TABLE MATERIAL SET aTY PER PRICE PER MAIN PARTS A/C A/C (USD) Component COMPAQ1 1 See SB Springs
5 DATE: Sep 21109 SERVICE BULLETIN No.: A3QQ-25-Q486 REVISION No.: 00 - Sep 21/09 Page: 1 Printed in FRANCE (iAIRBUS SAS. 2007. All rights reserved.EFFECTIVITY This Service Bulletin isapplicable to this (these) operator(s) : AFG F21 FLM lAW IRA IRB IRM OHY CONCURRENT REQUIREMENTS None REFERENCES' REPERCUSSIONS 

### TFU None DEB None 

### AOT None SIL None LINE MAINTENANCE AFFECTED 

### No LIFE LIMIT None OTHER None NATURE OFTHE WORK AIRCRAFT 

### YES EQUIPMENT 

### NO HARD 

### NO SOFT NO OBRM 

### NO MANPOWER Task250486-831-801-001: Modilication TOTAL MANHOURS 2.00 ELAPSED TIME (HOURS) I 2.00 PEN0ICES pendix . Elapsed Time Assumption 

### AP Ap

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep 21109 Page: 2 Printed in FRANCE OAIRBUS SAS. 2007. All righls feserved.

# ~A300 SERVICE BULLETIN SUMMARY
*'CONF ALL

Figure A-FSAAA - Sheet 01

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISIONNo.:00 - Sep21/09 Page:3 Printed in FRANCE ©AIRBUS S.A.S. Z007, All rights reserved.

# '$JA300 SERVICE BULLETIN SUMMARY
**CONF ALL



### 5 SPRING TO BE ADDED

DATE: Sep 21/09 I



### ~~ Figu·e A-FSAAA - Sheet 02
SERVICE BULLETIN No.: A300-25-0486 REVISIONNo: 00-Sep21/09 Page:4SERVICE BUL~ETIN AIRBUS CUSTOMERSERVICESDIRECTORATE 1 Rond PointMaurice Bellonte 31707 BLAGNACCEOEX FRANCE Tei: (33)561 933333 Telex: AIRBU 530526F Fax. (33)561 934251 ATA SYSTEM:25 

### TITLE: EQUIPMENT I FURNISHINGS· COCKPIT· DOOR MODULE

IMPROVEMENT MODIFICATIONNo,: 13545023270 This document conlains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property ofAIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the ~xpress condition that said document and the informationcontained in it shall betreated asconfidenti~l,shall not be usedfor any purposeotherthan thatforwhich itis herebydelivered. Itshall notbedisclosed inwholeorin part 10third partiesandshall not be duplicated in any manner (exceptfor the purposesof performingthe tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS priorwrittenconsent. 1. PLANNING INFORMATION dCONF ALL A. EFFECTIVITY NOTE: This Service bulletin is only applicable to aircraft on which the modified

intrusionand penetration resistantcockpitdoor isinstalled. (1) Models 82-203 B2K-3C B4-103 84-120' 84-203 B4-2C (2) Effectivityby MSN 00550079-008000820090009401280,1330135-01380151 015601600170 0175-01760180 0185 018701900192O~04022602390243-0244 025602990302 (3) Effectivityby Operator TheOperator/MSN relationship is providedfor informationonly and iscorrectatthetime of issue in accordance wah the informdtion available to AIRBUS. Any future changes resultingfrom transfer of an aircraftfromlone operatorto anotherwill not be reflectedin this list unlessthe Service Bulletinis revisedlor anotherreason.

5 

## OP61t1llt"/!,

AFG F21 FLM DATE: Sep 21/09 

### 01800190 I 0079 00940128013301350136013701560170 0243 0082015101760256 I SERVICE BULLETIN No..A300-25-0486 REVISIONNo..00 - Sep21/09 Page: 1 Printedin FRANCE toAIRBUS S.A.S.2007.All rights reserved.

# ($;A300 rRVICE BULLETIN 

### 'OPERA:rGR ,

# ',,", '-?l'


## - :'" 'MSN 'l;il 

# . 

# "' lAW 0239 I IRA 0080018$ 0187 0226 IRB 02990302 IRM 005500900160017502040244 OHY 01380192 (4) Configuration by MSN MS~ \", 00550079 0080 0082 0090 0094 0128 0133 0135 0136 0137 01380151 0156 0160 017b 0175 0176 0180 0185 0187 0190 0192 0204 0226 0239 0243 0244 0256 0299 0302 

## CONF'GURATION, 001 (5) Configuration definltion
standard configuration. Material Effectivity MATERIA~C~"'''' 

## "<ii' "i', QrY'~E~C;, S"EElji;J@TES" Component COMPAQ1 I 1 Consumable CMLAOl I As required HCONF 001 Contig 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a (6)

B. CONCURRENT REQUIREMEN+S None 

## c. REASON (1) History The A300 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 tape~ onthe doorframe. (3) Advantages Accomplishment ofthis serce Bulletinwill improve the cockpit door reliability. (4) Operational/Maintenance Consequences 

### None

5 DATE: Sep 21/09 REVISION No.: 00 - Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 Page: 2 ©AIRBUS S.AS. 2007. All rights reserved.SERVICE BULLETIN D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 250486-831-801-001: Modification (1) Install the Springs on the Strike ofthe Cockpit DOOf. E. COMPLIANCE (1) Classification RECOMMENDED (2) Accomplishment Timescale

F. Accomplishment of this Service Bulleti~ is recommended at the earliest opportunity

where manpower and facilities are available. 

### APPROVAL 

# l
Approved under EASA Design Organisation A proval No. EASA21J.031. If an aircraft listed in the effectivity has 

### a ~odification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airw9rthiness authority for any adaptation necessary before incorporation althe Service Bulletin. G. MANPOWER

I

~Task\2oQ~6t831,~t!01,iQO;L>:M

_ The manpower estimates given in this Service Bulietin 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 andtools, drying times for paints, sealants, etc., and general administration work are also not included. Get Access 0.50 OnAircraft Install the Springs on the Strike ofthe Cockpit Door. 0,50 Tests 0.50 Close-Up 

# I 0.50 TOTAL MANHOURS I 2.00 ELAPSED TIME (HOURS) I 200 I NOTE: For detail concerning the elapsed 1ime assumption, refer to Appendix -

Elapsed Time Assumption. H. WEIGHTAND BALANCE NotChanged 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep 21/09 Page: 3

# ~A300 SERVICE BULLETIN I.

J ELECTRICAL LOAD DATA Nol Changed 

### REFERENCES Aircrat! Maintenance Manual (AMM) 20 21 12 24-00-00 52-10 00 I 52·5H 1 Consumable Material Lisl (CML) I Elee. Std. Practices Manual (ESPM) 20-5500 Structural Repair Manual (SRM) I 51-30-29 

# I 52-51-11 PUBLICATION AFFECTED 

# I 1IIIustrated Parts Catalog (IPC) I INTERCHANG EABILITY /MIXAJILITY L. K.

NotApplicable M. SPARES None

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISIONNo: 00 - Sep21/09 Page:4 Printed In FRA~CE © AIRBUS SAS. 2007, All rights raservad.

# ~A300 SERVICE BULtETIN 2. MATERIAL INFORMATiON UCONF ALL A. MATERIAL· PRICE AND AVAILABILITY (1) Procurement Addresses This Service Bulletin isthe subject ofan AIRBUS monitored retrofitcampaign. Component COMPAQ1

(2) Price and Availability Customers with aircraft shown in the effectivity 01 this Service Bulletin should send a purchase order to AIRBUS. Quole the number of this Service Bulletin. The address is' I Airbus]Spares Support and Services Weg brim jaeger 150 0-22335 Hamburg Germany For ordering by internet: http://spares.8 irbus.com Forordering byfax: +49.40.50.76.25.90
NoAIRBUS kitwill be provided. Parts required to accomplish this 

## servici Bulletin can be manufactured by the operator following the Fig. A-FBBAA Sheet 01 orordered byaspare purchase order 10AIRBUS B. INDUSTRY SUPPORT INFORMATION Forthe 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 67 190622 E-mail: monltored.retrolit@airbus.com Fax: (33) 561 932745 Parts are at no charge forthe operator. The man-hours indicated inthis Service Bulletin will remain atthe operators' cost. 

### C. LIST OF COMPONENTS No Kit



### 5 DATE: Sep 21/09 SERVICE BULLETIN No.. A300-25-0486 REVISION No.: 00 - Sep 21/09 Page: 5

# I~A300 SERVICE BULLETIN D. LISTOF MATERIALS· OPERATORSUPPLIED (1) Consumable Materials Consumable CMLAOl ITEM DESCRIPTION 

# I REFERENCE TO CML QTY PERAle SEE MAT. No. NOTES Solvent General Purpose 11-026 As required Adhesive tape DAN269-25 1 (M) (2) Components Component COMPAQ1 ITEM NEW PART N' D'tY(UM) j<EYWORD ITEM OLD PART N° INT SEE

- I NOTES



## - 1 1183387 3 Spring

(3) Equipment 

### None E. PARTSTO BE HE-iDENTIFIEDBYOPERATOR 

### None F. TOOLING None

5 DATE: Sep 21109 SEAVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep 21109 Page: 6 Printed in FRANCE 

### eAIRBUS SAS. 2007. All rights reserved.

# ~A300 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 250486·831-801-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED INTHE REFERENCED PROCEDURES. Al'\NAY$ OBEY THE DAECAUTIONS THAT FOL.
.OW TO KEEP ELECTR,CAL W1R:NG IN A SATiSFACTORY C01>JDlTlON ;ELE·':;FUCA.LLY AND MECHANiCALL't SERVICEABLE) WHEN YOU DO MAINTENAt'>lCE WORK. REPAIRS OR MODIFICATiONS. /o:lWAYS KEEP El.ECTRICfi,L WIRING, COMPONENTS AND THE WOR~ AREA AS CLEAN AS POSSIBLE TO DO THIS: I PUT PROTECTION, SUCH AS PLASTiC SH[EnNG. CLOTHS, ETC" }\S NECESSARY ON WIRING AND COMPONENTS REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAl.. AND OTriER CONTAMINATiON THESE PRESAUTiONS WilL DECREASE THE. RISK OF CONTAM,I\ATi01'J AND DAMAGE TO THE ELECTRICAL WIR(NG INSTALLAT!ON IN CASE OF CONTAM,NATION REFER TO ESPM 2055 00 Task Associated Data



### A. Zone't.- 210 220 Access 

## - - - Door 1831

,," Manpow~r, 

## - 

# ••

- 

# -

- TOTAL MANHOURS 2.00 ELAPSED TIME (HOURS) 12.00 GENERAL (1) Subtask 250486-910-002-001 - Standard Practices 'Manpower He~Durces Skills Material necessary

## to dothejob , 

### -

## - NON SPECIFIC
Consumable CMLA01 ITEM DESCRIPTION REFERENC~ T~

_ QTY PER

### Me SEE CML MAT. No. NOTES Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-21-12 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep 21/09 Page: 7 Printed in FRANCE @AiRBUS S,A.S. 2007. All rights reserved.

# I~A300 rRVleE BULLETIN 

### Bl;{~rence~,:Jl} Consumable Material List (CML) Structural RepairManual (SRM) 51-30-29 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML).
As required

Skills 

# INON SPECIFIC in this 8. PREPARATION

I I

# IAIRFRAME I I I 

### :~'·J:~,er\W~es0u.rpe'S I I (1) Sublask 250486-941-001-0,01 - Job Set-up 

### I I <*'.",;L

## J,No~J:0nes,ahcrAcc'ess?:'P}ln"eJ§

AccessZWo~jS}:i~!®.,'1lf0:_

Skills 

## --'" :~ 11?)~renGEts I Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 I 52-10-00, Page Block 001 

### I I (a) Make surethat the a'reraftis electricallygrout')ded(Reier to AMM 24-00-00, Page Block 301). (b) Putaccess platform in position I (e) Open the passenger/crew door 831 (Refer 10AMM 52-10-00, Page Block001).

5 DATE: Sep 21/09 SERVICE BULLETIN No.:A300-25-0486 REVISIONNo: 00· Sep21/09 Page:8 Printed in FRANCE ©AIRBUS S.A.S. 2007, All rigllts reserved,

# ~A300 SERVICE BUJETIN C. PROCEDURE (1) Sublask 250486·831-001-001 - lnstail the Springs on the Strike of the Cockpit Door.

" Work:

### Zones and Acc.ess Panels " Zone 

## ';C" . AccesslWork location 210 220 Access 

## IDoor 831

. 

# ." Manpower Resources 

# '. Manhours 0.50 Minimum number of person 1 Subtask elapsed time 

# , 050 Skills AIRFRAME Material necessary 10do the job Component COMPAQl ITEM NEW PART N' QTY (UM) KEYWORD SEE"'"

. 

### ; 

## ~. NOTES 1 1183387 

### 3 Spring Consumable CMLAOl ITEM DESGRIPTIGN 

### r Adhesive tape REFERENCETO QTYPERAle CML MAT. No. DAN269-25 1 (M) 

# s~~ NOTES



# "
_

References 

### "c' 

# .,;, " 

# ,- 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 Sprinps
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 

### NOTE: DATE: Sep 21109 SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep 21109 Page: 9 Printedin FRANCE @AJRBUSSAS.2OO7.A1lrightsreserved.

# ~A300 rRVICE BULLETIN The springs item 1 can be manufactured by the operator following the Fig. A-FBBAA Sheet 01 or ordered by a spare purchase order 

### to AIRfUS (c) Apply onthe doorthe !AdhesIVetape on all surface Incontact between the door and the springs Item 1 I Adhesive tape DAN269-25 1 {M} D. TEST



# - Door 831 

# ,<J~er R~p.u"rces ~,

## j,:

AIRFRAME Access 

### Zo.ne 2tO 220 (1) Subtask 250486-700-001 "Of1
-Testing



## lWbJW:~one§;a-rld:'7\i!ce'ss P-a-rfell,s



### Acc.essiWor-KI68ijilpJl

Skills 

## Referer¢e's AircraftMaintenance Manual(AM~) 52-5H 1, PageBlock501

I (a) Checkthatthe cockpit dooroperates properly byopening/closing it several times.

- Ifthe door is IOU~dhard to open (orclose!),dothe adjustment ofthe door gap (Refer to AMM 52-51-11, Page Block 501). E. CLOSE"UP

AIRFRAME - Close-up

I I I 

## ",:-srtlanpMter>R!rs9uFoes ~ I I Skills

•. j. 

## F.l¢Jii&tLQi ~ Aircraft Maintenance Manual (AMfvl) 52-10-00, Page Block001 (a) Make sure that the fork areas are clean and clear of tools and other items of equipment. I (b) Closethe passenger/crew 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 REVISION No.. 00 - Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 Page: 10 ©AIRBUS B.A.S. 2007. All rights reserved."CONF ALL

5 DATE: Sep 21109 Figure A·FBAAA •Sheet 01 Installation of Springs on the Strike ofthe Cockpit Door SERVICE BULLETIN No.: A300-25-0486 REVISION No: 00- Sep 21109 Page: 11 Printed in FRANCE €:IAIRBUS S.A.S. 2007. All rights reserved.

# ~A300 SERVICE BULLETIN

··CONF ALL 

## BEFORE

[2}

FigureA-FBAAA - Sheet 02 Instaliation of Springs on the Strike ofthe Cockpit Door 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep21109 Page: 12 Printedin FRANCE C AIRBUS SAS. 2007.All rightsresewed.SERVICE BULtETIN



### hCONF 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 21/09 Figure A~FBAAA-Sheet 03 Installation of Springs on the Strike ofthe Cockpit Door SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 -Sep 21109 Page: 13 Printed in FRANCE 

### eAIRBUS S.A.S. 2007. All rights reserved_

## '$;A300 SERVICE BULLETIN

"CONF ALL PRINCIPLE OF MANUFACTURE

10mm 10.394 In) l.gmm (0.075 in) 

# Ai R.Wmm (0.384 ;n)DIAM. 9,91 mm I 

# 1

(0,390In), I , 

# . 

# 1"'""1 .~- I '"0' 

# .--t(:';::,~, 

# ~-~

~ I 377mm 3mm ~_-.-L_ 

# :±=::~==_

'~~ (14M,nl 152 -(0118,") 

# =••L-L~_' 

# 41,-(~":_:'~1_-------

~ 2~ A ~~~ 

# ,,~ (0.7B7 in) OIAM. 5.82 mm 10..229In)



## A-A

:m.2mm (1.169 inl 83,5,"m {2,500Inl 

# "o.mm('~

(0,a16inl _~_

, --1- 

### '""

'm" (o..197 in) 40.2 mm

(1.583 In) MATERIAl ASNA3322OR --------_AMS551BOR
-- 1.4310. THICKNESS o..4m'" (o.,157in) IDENTIFICATION IDENTIFY Tf-lESPRING WITli PART NUMBER'1a3357 NOTE, NOT SPECIFIED RADIUS; R. 3mtn (a,llS in)
A_S8_28J.'""_S_BBAA_"'_"2 Figure A·FBBAA - Sheet 01 Principle af Manufacture 0.1the Springs 

# , DATE, Scp 21109 SERVICE BULLETIN No.: A30Q·25-048S REVISIONNo,' 0.0- Sep21/09 Pags: 14 Prin'oo InFflANC~ © AIRBUSSAS. 2007. Allilghl' re,orvoo.

# ~A300 SERVICE BULLETIN Appendix - Elapsed Time Assumption **CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A300-25-0486



### STEPS MH ET PER

GET ACCESS 0.50 0.50 1 

### I 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

I I I I 0 0.5 I 1.5 2 ELAPSED TIME TOTAL MAN HOURS (MH) 2.0 (HOURS) ELAPSED TIME (El) 2.0

MH: MAN HOURS ET: ELAPSED TIME PER: NUMBER OF PERSONS NOTE: 

# 6~~R~~~~~I~~~6~¢E~~~~~~~~T ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM.

Figure A-FAAAA - Sheet 01 Appendix - Elapsed Time Assumption 5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISIONNo.:00-Sep21/09 Page: 1 Printed in FRANCE iDAIRBUS SAS. 2007. All rights reserved.

# ~A300 SERVICE BULLETIN REPORTING SHEET 

### TITLE: EQUIPMENT 

### I FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT MODIFICATION No.: 13545023270 Please complete the appropriate item (A or B): A-58 WilL BEembodied YES/NO(if NOplease comment) II YES, aircraft concerned (as per S8 effectivity by default) and planned dates (monthlyear) of embodiment:

B . 58 HAS BEEN embodied on aircraft: Operator comments: From Airline: NamefTitle: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this 58): If information is needed prior to next normal revision or prior 10S8 embodiment, please indicate required service(s): Either: ModificationOperational Impact(MOl), if available YES/NO Or : Intermediate revision 

# I YES/NO 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 Updating of maintenance documentation to show pre and post SB data. • Updating of maintenance and operatidnal documentation to show post SB data after embodiment. II this SB requires previous or simultaneLs accomplishment 01 other SBs, Airbus shall automatically include them in the manual revisions. Reldr to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellante 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 932806 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

5 DATE: Sep 2t/09 SERVICE BULLETIN No.: A300-25-0486 REVISION No_: 00 - Sep 21109 Page: 1 Prinleo in FRANCE 

### eAIRBUS S.A.S. 2007. All riglllsreserved.

# ~A300 SERVICE BULLETIN QUALITY PERCEPi'ON FORM Use this form 10tell us what is your perception of the quality 01this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve thequality of our Service Bulletins. I We thank you for the time you have taken in completing IthiS form. (Please rate on a:scale of 1 to 4, with 4 being the highest score)

- Quality rating ofthis S8

- Quality rating of the Accomplishment Instructions

- Quality rating ofthe Illustrations

- Isthis S8 easy to understand? 

### 4 3 4 3 4 3 Y/N 2

2 2
Ifyou have had difficulties in the accomplishment ofthis 88 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: NamelTiUe: Please return thistorm toAIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellante 31707 BLAGNAC CEDEX FRANCE Atln : SEM4 Service Bulletins Management FAX: (33) 561 934251 Orvia your Resident Customer Support Office. Date:

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486 REVISION No.: 00 - Sep 21/09 Page: 1 Printed in FRANCE © AIRBUS S.A.S. 2007, All rights reserved.