# ~A380 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond 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 f 

### FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT ··CONF ALL MODIFICATIONS MODIFICATION CLA$SIFICATION MAJOR INane MINOR 

## I69934T79040 

## 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 ofthe product. AUother changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES The A380 aircraft in-service experience has shown that cockpit door installation must be improved. This Service Bulletin recommends to modify the COlkPit door installation by adding springs adhesive tapes on the door frame. I 

# ::~:::::::Lo~~~:os:rviceBUlietin willImprovetheICOCkPit doorreliability. and

I E;VALUATION TABLE COMPLIANCE RECOMMENDED CANCELS INSPECTION SB 

### NO POTENTIAL AD 

### NO AIC OPERATION AFFECTED 

### NO RELIABILITY AFFECTED 

### NO PAX COMFORT AFFECTED 

### NO COST SAVING 

### NO LROPS AFFECTED 

### NO STRUCTURAL LIFE EXTN 

### NO VENDOR 58 INVOLVED 

### NO MATERIAL PRICE INFORMATION MATERIAL PRICE INFOfjlMAT10N TA8LE MATERIAL SET QTY PER PRICE PER MAIN PARTS AlC AlC (USD) Component COMPA01 1 See 5B Springs
5 DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-8058 REVISION No.: 00 - Sep 21109 Page: 1 Printed in FRANCE (')AIRBUS S.A.S. 2007. All rights reserved.

# ~A380

EFFECTIVITY SERVICE BULLETIN I SUMMARY 

# I This Service Bulletin is applicable to this (these) operator(s) : AFR QFA SJA UAE CONCURRENT REQUIREMENTS 

### None REFERENCES I 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 Task 258d,58-831-S01-001: Modification TOTAL MANHOURS I 2.00 ELAPSED TIME (HOURS) I 2.00 PENDICES endix - Elapsed Time Assumption 

### AP App

5 DATE: Sep 21/09 SERVICE BUllETIN No.: A380-25-B058 REVISION No: 00 . Sep 21109 Page: 2 Printed in FRANCE €:IAIRBUS SAS. 2007. All rights reserved.SERVICE BULLETIN 

### SUMMAT
**CONF ALL



### A

5 DATE: Sep 21/09 REVISION No,; 00 - Sep 21/09 Figure A-FSAAA Sheet 01
SERVICE BULLETIN No.: A380-25-8058 Page: 3 Printed in FRANCEhCONF ALL 

# ~A380 ERVICE BULLETIN SUMMARY



### I 

# ~@] Fi9UL A-FSAAA - Sheet 02 SPRING TO BE ADDED

5 DATE: Sep 21/09 REVISION No :00 - Sep 21/09 SERVICE BULLETIN No.: A380-25-8058 Page: 4 ©AIRBUS S.A.S. 2007. All rights reserved.

# ~A380 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 ATA SYSTEM: 25 

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

IMPROVEMENT I MODIFICATIONNo.: 69934T79040 

# I This document contains AIRBUS PROPRIETARY INFORMATION and shall at all limes remain the property at AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any informationcontained in it. It is delivered on the express condition that said documentand the information contained in

### it shall be treated as confidential, shall nol be used for any purpose other than that forwhich it is hereby delivered. Itshall not be disclo~ed inwhole or in part tothird parties and shall 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 priorwritten consent. 1. PLANNING INFORMATION HCONF ALL A. EFFECTIVITYThis Service bulletin is only applicable to aircraft on which the modified

intrusion and penetration resistant cockpit door is installed. , (1) Models 380-841 380-842 380-861 (2) Effectivity by MSN 00030005-00080010-00170019-00230025-00270029 0033-0034 0040 0045 (3) Effectivity byOperator The Operator/MSN relationship is provided for information only and is correct atthe 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 foranother reason. 

### I !"OPERAI0}l.'j .

### , I , 

### .j".'"'"

## '.I\I$I'I""w 

## l'" . 

# •. AFR 00330040 OFA 0014 0015 0022 0026 0027 0029 SIA 000300050006 0008 0010 0012 0019 002100340045 UAE 00070011 001300160017002000230025 5 DATE: Sep 21/09 SERVICE BULLETIN No..A380-25-8058 REVISION No .00 - Sep 21/09 Page: 1 Printed ill FRANCE © AIRBUS SAS. 2007. All righls reserved.

# ~A380 SERVICE BULLETIN I (4) Configuration by MSN MStil \ 00030005000600070008001000110012001300140015 00160017001900200021[ 002200230025 0026 00270029 0033 0034 0040 0045 (5) Configuration definition ,GONFIGURATI@N 001



### dCONF 001 Config. 001 is valid for all

# Ire aircraft given in the effectivity of this Service Bulletin as a standard configuration. I (6) Material Effectivity 

## MI!1:8"i4()f'l'~"Rl\lJ'iSEE NQTES Component COMPAOl I 1 Consumable CMLA01 I As ,required I B. CONCURRENTREQUIREMENTS None C. REASON (1) History The A380 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~ on the door frame. (3) Advantages I Accomplishment of this selice Bulletin will improve! the cockpit door reliability. (4) Operational/Maintenance Consequences I None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to: I Task 258058-831 "801-001. Modification (1) Install the Springs on tt Strike of the Cockpit D'oor.



### 5 DATE: Sep 21/09 SERVICE BULLETIN No.. A380·25·8058 REVISION No.: 00 - Sep 21/09 Page: 2 Prirtled in FRANCE ©AIRBUS SAS. 2007. All rights reserved.E. COMPLIANCE (1) Classification RECOMMENDED (2) AccomplishmentTimescale Accomplishment of this Service BuUetinis recommended at the earliest opportunity where manpowerandfacilities areavailable. F. APPROVAL Approved under EASADesignOrganisationApproval No. EASA21J.031. If an aircraft listed in the effectivity has a modification or repair embodied Ihat is not of AIRBUS origin, and which affects the content of this Service Bullelin, the operator is responsiblefor obtaining approval by its airworthinessauthorityforany adaptation necessary beforeincorporationofthe Service Bulletin. G. MANPOWER The manpower estimatesgiven in this Service Bulletin are based on the direct laborcas! to dothe work. These estimates assumethatthe work will be done byexperienced personnel, and mayneed to be revised upwardsto suit operator's circumstances. The estimatesdo not include the time 10prepare, plan or inspectthe work. Manufactureand procurementof parts and tools, drying timesfor paints, sealants, etc., andgeneral administrationworkarealso no! included. .:Task 25805_8-831-801-001; Modification GetAccess 0.50 On Aircraft I Installthe Springsonthe StrikeoftheCockpit Dqor. 0.50 Tesls I 0.50 Close-Up I 0.50 TOTAL MANHOURS 2.00 ELAPSEDTIME (HOURS) 2.00

For detail concerning the elapsed lime assumption, refer to Appendix - ElapsedTimeAssumption. H. WEIGHTANDBALANCE NotChanged I. ELECTRICALLOADOAT A NotChanged 

### J. REFERENCES Aircraft Maintenance Manual (AMM) 20·21·11 52-51-11 24-41-00 52-10-00
5 DATE:Sep 21/09 SERVICE BULLETIN No.:A380-25-8058 REVISION No.: 00 -Sep21/09 Page:3 Printedin FRANCE CAIRBUSSAS. 2007.All rights reserved.

# '$,A380 SERVICE BULLETIN Consumable Material list (CML) I Elec. Std. Practices Manual (ESPM) 20-551~OO Structural Repair Manual (SRM) I . 51-42~OO I 52-51

# tl1 I PUBLICATION AFFECTED

Not Applicable I IIllustrated Parts Catalog (IPe) I INTER CHANG EABILITY /MIXAJILITY I 

### L. K.

M. SPARES None



### 5 DATE: Sep 21/09 SERVICE BULLETIN No,: A380-25-8058 REVISION No.: 00 - Sep 21/09 Page: 4 Printed in FRA!,!CE ©AIRBUS S.A.S. 2007, All rights reserved.2. MATERIAL INFORMATION **CONF All A. MATERIAL· PRICE ~NDAVAilABILITY I (1) Procurement Addresses

I This Service Bul1letin is the subject of an tlRBUS monitored retrofit campaign. Component COMPA01I Custom

# J' ers with aircraft shown in the effecti lity 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 D-22335 Hamburg Germany For ordering by internet: http://spares .airbus .com For ordering by fax: +49.40.50.76.25.90 , (2) Price and Availability No AIRBUS kit will be provided. 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 SERVI8ES DIRECTORATE 1 Rand Point Maurice Bellonte 31707 BLAGNAC CEDEX France Tel: (33) 5 67 190622 E-mail. monitored.retrofit@airbus.com Fax: (33) 5 61 932745 Parts are at no charge lor the operatoL The man-hours indicated in this Service Bulletin will remain at the operators' cosl. C. LIST OFCOMPONENTS No Kit

5 DATE: Sep 21109 REVISION No: 00 - Sep 21/09 Printed In FRANCE SERVICE BULLETIN No.: A380-25-8058 Page: 5 I ©AIRBUi S.A.S. 2007. All rights reserved.

# ~A380 SERVICE BULLETIN 

### D. LIST OF MATERIALS -OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLAOl
Solvent General Purpose Adhesive tape (2) Components As required 

## '1M) Component COMPAQ1 

## IT~MNEWlPriRhf111i~, 'K~J:,,,,.fiii~' h:&,,'" 1183387 (3) Equipment None E. PARTS TO BE RE·IDENTIFIED BYOPERATOR 

### None F. TOOLING None

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-B058 REVISION No.. 00-Sap21109 Page:6 Printed In FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### 3. ACCOMPLISHMENT INSTRUCTIONS Task 258058-831-801-001 - Modification WARNING: MAKE SURE THAT YOU OBEY AUl THE WARNINGS AND All THE CAUTIONS

INCLUDED INTHE REFERENCEOIPROCEDURES. ALWAYS 08EY TH PREJAUTIOI'JS H11\T FOLi
..OW Te KEFT"' ELECTRiCAL W1FU\C; iN fA. S,'nlscACTORY CONDiTiON :,ELECTRiCALLY AND MECH,D,fJ:CAllV SERVICEABl.'::). WHEN YOU DO ivl/,INTEN/\NCt=: WORK, REPAIR'SOR \10DiF1CATiONS. ftUl\,t"AYS KEEP ELECTRICAL WIRING, co~.opmJFI\TS ,'\ND THE WOEK AREA AS CLEAN AS POSSiBL.E TO DO THiS: PUT PROTECTION, SUCH ASI PLASTIC SHEETING NECESSARY ON WIP,iNG AND C()MPONENTS. ETC; AS REGULARLY REMOVE ALL SHAfJ

1iNGS, UN\i>1Ai\lTEO~"lArEP:AL r\\lD OTHER CONTAMlt'-lATIQN. 

# I THESE fi'RECAUTIONS Will DECREASE THE RiSK OF CONTAMINATIOi'J AND GA\llAGE TO THE ELECTRICAL WIRING INSTAllATION.

Task Associated Data

TOTAL MANHCUR$ ELAPSED TIME (HOURS) 210 220 

### " ..~'''''£;i:~. ',Acces~



### MIL I Door

A. GENERAL (1) Subtask 258058-910-001·001 . Standard Practices 

# Is~~r~I£;I~~

# ·~··I

~: -~ 'p' 

### Refererid~~ Aircraft Maintenance Manual (AMM) Task 20·21-11-911-801 5 DATE: Sep 21/09 SERVICE BULLETIN No. A380-25-8058 REVISION No,: 00 -Sep 21/09 Page: 7 I Printed In FRANCE © AIRBusl S.A,S. 2007, Ail rights reserved. I

# ($A380 SERVICE BULLETIN

Consumable Material List (CML) Structural Repair Manual (SRM) (a) For the specification Material List (CML), of the I 51-42-00 I malerial numbe~s (Mat. No,), refer to Consumable (b) Cleantheworkareawith: Solvent General 11-026 As required 

### purpose: I (c) Forthe removal and Installation offasteners (Referto SRM 51,42-00) (d) To torque lighten the standard threaded fasteners (Refer 10 AMM Task 20-21-11-911-801 ). (2) Subtask 258058-839-001-001 -Administrative '.~ Skills 

### J~!nRQ~E[tf.lelfWrc~s 

## jI NON SPECIFIC Write in the applicable aircraft records that you

# h6ve done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 258058-941-001-001 - Job Set-up

(Refer to AMM Task 

### Wor:Kjl:onesabd,Ac~?p.a:tJet.;' , f'; ,_ 

## ! Acci:{§'$"N¥prl(.J?:lqaJioir ' I I I 

### Zone 210 220 ~n'p~elj~QutcesSkills I AIRFRAME I 

### Referer1~s'
- I Aircraft Maintenance Manual (AMM) Task 24-41-00-860-801 I Task 52-10-00-010-801 (a) Make sure that th~ aircraft is electricallJ grounded 24-41-00-860-801). I

I (b) Put access platform in position (c) Open the passenger/crew door M1L (Refer to AMM Task 52-10-00-010-801).

5 DATE: Sep 21109 SERVI,CE BULLETIN No.. A380-25-8058 REVISIONNo,:00-Sep21/09 Page:8 I Printed in FRANCE © AIRBUS SAS, 2007. All rights reserved.I 

# ~A380 SERVICE BULLETIN C. PROCEDURE (1) Sublask 258058-831-001-001 - Install thel Springs on the Strike 01the Cockpit Door.



## , Work lones and Ac<;:ess Panels Zone , AccessfWork location 210 220 Access IDoorM1L ~anpower Resources Manhours 

### 050 Minimum number 01 person 1 Subtask elapsed time I 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEWPARTN"L QTY IUM) KEYWORD 

### SEE"

~, 

## - NOTES 1 1183387 3 Spring Consumable CMLAOl ITEM DESCRIPTIG~t

Adhesive tape REFERENCETO QTY PERAle CML MAT.\Jo. DAN269-25 1 (M) SEE NOTES 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 - Princiole of Manufacture of the Springs
6


### 3
6 

## lal Remove:

Screw 

## (bl [nstall . Spring 1183387 and attach with . Screw [lem (2)
Item 1 [tern (2) Retain

Retained at removal


### 5 NOTE: DATE: Sep 21109 SERVICE BULLETIN No_:A380-25-8058 REVISION No_:00 -Sep 21/09 Page: 9 PonIed in FRANCE e AIRBUS SAS. 2007. All rights reserved_

# I$A380 SERVICE BULLETIN The springs item 1 can be lered by a spare porchase order to AIRBUS or manufactured 

# bY the operator following the Fig. AFBBAA Sheet 01, I (c) Apply on the doortheIAdheslvetape on allsurface Incontact between thedoorand the springs Item 1 I Adhesivetape DAN269·25 1 (M), D. TEST


## 1*'7or1e'"

210 220 (1) Subtask258058-700-001-001 -Testing



## ~:J:rK:!lone~A(

iAc~e 

# ahe1$r:f' !'Ii'At'Ces~ork16qi(ioh

I AccessI DoorM1L I I



### . ''i'.appoyver }le.sou~~~'
- Skills I AIRFRAME I 

## ~. ~, I/,,,~ilfen<r~" ' AircraftMaintenanceManual(AMM) Task52-5H 1-820-801 (a) Check that the cockpit door operates properly Jy opening/closing il several times. I Ifthe door is found hard to open {or close, do the adjustment ofthe door gap (Refer to AMM Task 52-51-11-820-801).



### 0rk

## llpnes0and'<ct:ess;~a'r!el~ 'I '"'~t~e~~:0fiIo[15:~jqqatT0n'~" I I I 210 220 (1) Subtask 258058-942-001-001 - Close-up



### I

SkHls I AIRFRAME I

5 

## Be'~tt~n.ce§Jqy, Aircraft Maintenance Manual (AM,M) Task 52-10-00-~10-801 (a) Make sure that the lark areas are clean a~d clear of tools and other items of equipment I I (b) Close the passenger/crew door831 (RefertoAMM Task 52-10-00·410-801). I (c) Remove the access platform. (d) Restore the systems Ld the aireraftto normal operating condition. DATE: Sep 21/09 I SERVICE BULLETIN No,' A380-25-8058 REVISION No..00 - Sep 21/09 Page: 10 Printed in FRANCE ©AIRBUS S.A.S. 2007. All righls reserved.··CONF ALL

5 DATE: Sep 21/09 Figure A-FBAAA . Sheet 01 Installation ofSprings on the Strike ofthe Cockpit Door SERVICE BULLETIN No.: A380-25-8058 REVISION No.: 00 . Sep 21109 Page: 11 Printed ill FRANCE 

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

# $A380 SERVICE BULLETIN
~"'CONF

ALL 

## BEFORE

(2)

Figure A-FBAAA -Sheet 02

Installation of Springs on the Strike ofthe (!;ockpil Door

I I 5 DATE:Sep 21/09 SERVICEBULLETINNo.:A380-25-8058 REVISION No:00 - Sep 21/09 Page: 12 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.**CONFALL

(2) 

## AFTER.

~ A-A APPLY ON THE DOOR THE ADHESIVE TAPE DAN 269-25 ON ALL SURFACE IN CONTACT BETWEEN THE DOOR AND THE SPRINGS.

COCKPIT DOOR

5 DATE. Sep 21109 Figure A-FBAAA - Sheet 03 Installation of Springs on the Strike ofthe Cockpit Door I I SERVICE BULLETIN No:A380-25-8058 REVISION No.:00 -Sep21/09 Page: 13 Printed In FRANCE © AIR8US'SAS. 2007, All rights reserved.

## ,!;;A380 SERVICE BULLETIN

"CONF ALL PRINCIPLE OF MANUFACTURE 

# Ai ,'mm,-++- {O.07SI": 

# II 10 mm 

# I 'm'"'~,"1

__ Zl.8mm 37,7 mm (0.85S ioj 

# "'1''"I"'~" 

# yr"';:;~"--.1 S:{j(~~~~mm 

# _,~/_I"_' _"

__ '

_ (0.079 In) 

## ~- 

# A-l RIOmm ,10.394 In)OIAM, 9,91 rn'"

# I

(0.390 in). 

# , f--n;mm-l I IO.9~5in) 

### t

# I 

# -+~~:F=-+~

lOmm a,3llim' 

# I ====~_IO~:r~~:12~n:~_ ._=-= 20m01 (0,787;n) OIAM. 5,82 mm (0,229 in)

S3.5mm 12.500 in) A-A

THICKNESS 0.4 n1n1jO.157 In) IDENTIF!CA nON IOENTIFY THE SPRING WITH PART NUMBER'IS3387 MATERIAL ASNA3322 OR AMS5518 OR 1.4310

L_SB_Z£8058_5_BllAA_"'_"' NOTE: NOT SPECIFIED RADIUS: R= 3 Inm (0,118 In) ~ I " ,/ R.OAmm

~ ~

_ """"" I (0,""'1 " (~_ 

# --w (0,02910)' 

# --w I -'T' 

# ~,_j ,"omm 

# '-'---rl---,-~t'

"T"

---~~ I 5,nm (0.197 In) lOmm 

# --~- 'I (0.394 in)

. a 83.5mm (3.287in) UNFOLD 30,2 mm (1.18S;n)

Figure A·FB8AA· Sheet 01 Principle 01Manufacture of the Springs 

# , DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-8058 REVISIONNo.:00· Sap21109 Page: ,4 1"'",1"" in FFlANCE '" AIRBUS SA-S, 200" Allrlg~lS reservEd.

# ~A380 SERVICE BULLETIN Appendix - Elapsed Time Assumption
*"CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A380-25-8058

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

I I I I 0 05 I 1.5 2 ELAPSED TIME TOTAL MANHOURS (MH) ELAPSED TIME (El) 20 20 (HOURS)

MH:MANHOURS ET: ELAPSED TIME PER: NUMBER OF PERSONS NOTE: THIS CHART ISONLY 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 21/09 SERVICE BULLETIN No.: A380-25-8058 REVISION No: 00 - Sep 21/09 Page: 1 Printed i[l FRANCE ©AIRBUS SAS. 2007. All rights reserved.

### TITLE: 

# ~A380
EQUIPMENT IFURNISHINGS - COCKPIT - DOOR MODULE IMPROVEMENT MODIFICATION No.: 

### 69934T79040 Please complete the appropriate item (Aor B): A. S8WILLBEembodied YESINO(if NOpleasecomment) If YES, aircraft concerned (as per 58 eHectivity by default) and planned dates (monthlyear) of embodiment:

B - 58 HAS BEEN embodied on aircraft: Operator comments: From Airline: NamefTitle: Signature: Date:

YES/NO YESINO Ifoperational documentation is affected (see Paragraph 1.Kofthis S8): Ifinformation is needed priorto next normal revision or priorto S8 embodiment, please indicate required service{s): Either: Modification Operational Impact (MOl), if available Or : Intermediate revision Important Information: This S8 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 5B data.

- Updating of maintenance and operatiohal documentation to show post S8 data after embodiment. If this S8 requires previous or simultaneLs accomplishment of o~her SBs, Airbus shall automatically include them in the manual revisions Refe~ to SIL 00-037 for detail~d information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Altn: 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 21/09 SERVICE BULLETIN No_: A380-25-8058 REVISION No : 00 - Sep 21109 Page: 1 PrintedinfRANCE CAIRBUSS_A.S.2007. Allriglltsleserved.

# !$;A380 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this 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 the quality ofour Service Bulletins. We thank youfor the time you have taken in completing this form. (Please rateon ascale of 1 to 4, with 4 being the highest score)

-Quality rating ofthis 58

- Quality rating of the Accomplishment Instructions

- Quality rating 01 the Illustrations

- Isthis 58 easy to understand? 4 3 4 3 

### 4 3 Y/N 2

2 2
Ifyou have had difficulties in the accomplishment of this 58 please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kitcontent X Preparation X Reason X Listof Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re"identitication X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: NamefTitle: Please return thisform to. AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rend Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Atln SEM4 Service Bulletins Management FAX (33) 5 61 934251 Orvia your Resident CustomerlSupport Office. Dale:

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-8058 REVISION No.: 00 - Sep 21/09 Page: 1 Printed in FRANCE ©AIRBUS SAS. 2007. All rights reserved.