~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 of the 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 willImprovethe ICOCkPit door reliability.

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 QF A 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 OF THE 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 FRANCE
hCONF 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) 5 61 933333

Telex: AIRBU 530526F

Fax: (33) 5 61 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 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 nol be used for any purpose other than

that for which it is hereby delivered. It shall not be disclo~ed in whole or in part to third 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 prior written consent.

1. PLANNING INFORMATION

HCONF ALL

A. EFFECTIVITY

This 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 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.

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 0027 0029

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. CONCURRENT REQUIREMENTS

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) Accomplishment Timescale

Accomplishment of this Service BuUetin is recommended at the earliest opportunity

where manpower and facilities are available.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.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

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

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cas! 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 10prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also no!

included.

.:Task 25805_8-831-801-001;Modification

Get Access 0.50

On Aircraft I

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

Tesls I 0.50

Close-Up I 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

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

Elapsed Time Assumption.

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD OATA

Not Changed

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 - Sep 21/09 Page: 3

Printedin FRANCE C AIRBUS SAS. 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

52-51tl1

I

PUBLICATION AFFECTED

Not Applicable

I

I Illustrated 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 ~ND AVAilABILITY

I

(1) Procurement Addresses

I

This Service Bul1letin is the subject of an tlRBUS monitored retrofit campaign.

Component COMPA01I CustomJ'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 OF COMPONENTS

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~M NEWlPriRh f111i~,

'K~J: ,,,,.fiii~' h:&,,'"

1183387

(3) Equipment

None

E. PARTS TO BE RE·IDENTIFIED BY OPERATOR

None

F. TOOLING

None

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-B058

REVISION No.. 00 - Sap 21109 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 IN THE 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'S OR \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

1

iNGS, 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~

Door MIL I

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) Clean the work area with:

Solvent General 11-026 As required

purpose: I

(c) For the removal and Installation of fasteners (Refer to 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 j

I 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 M1 L (Refer to AMM Task 52-10-00-010-801).

5 DATE: Sep 21109 SERVI,CE BULLETIN No .. A380-25-8058

REVISION No,: 00 - Sep 21/09 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 01 the 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 PER Ale

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 door the IAdheslve tape on all surface In contact between the door and

the springs Item 1 I

Adhesivetape DAN269·25 1 (M),

D. TEST

1*'7or1e'"

210

220

(1) Subtask 258058-700-001-001 - Testing

~:J:rK:!lone~A( iAc~e ahe1$r:f'

!'Ii'At'Ces~ork16qi(ioh

I

Access I Door M1L I

I

. ''i'.appoyver }le.sou~~~' -

Skills I AIRFRAME

I

~. ~, I/,,,~ilfen<r~" '

Aircraft MaintenanceManual (AMM) Task 52-5H 1-820-801

(a) Check that the cockpit door operates properly Jy opening/closing il several times.

I

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).

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 door 831 (Refer to AMM 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 of Springs on the Strike of the Cockpit Door

SERVICE BULLETIN No.: A380-25-8058

REVISION No.: 00 . Sep 21109 Page: 11

Printed ill FRANCE e AIRBUS S.A.S. 2007. All rights reserved.
$A380

SERVICE BULLETIN

~"'CONFALL

BEFORE

(2)

Figure A-FBAAA - Sheet 02

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

I I

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-8058

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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
**CONF ALL

(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 of the Cockpit Door

I I

SERVICE BULLETIN No : A380-25-8058

REVISION No.: 00 - Sep 21/09 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

(3.287 in)

UNFOLD

30,2 mm

(1.18S;n)

Figure A·FB8AA· Sheet 01

Principle 01 Manufacture of the Springs

, DATE: Sep 21/09 SERVICE BULLETIN No.: A380-25-8058

REVISIONNo.: 00· Sap 21109 Page: ,4

1"'",1"" in FFlANCE '" AIRBUS SA-S, 200" All rlg~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 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

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 I FURNISHINGS - COCKPIT - DOOR MODULE

IMPROVEMENT

MODIFICATION No.: 69934T79040

Please complete the appropriate item (A or B):

A . S8 WILL BE embodied YESINO(if NO pleasecomment)

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

If operational documentation is affected (see Paragraph 1.K of this S8): If information is needed prior to

next normal revision or prior to 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

Printed in fRANCE C AIRBUS S_A.S. 2007. Allrigllts leserved.
!$;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 of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this 58

- Quality rating of the Accomplishment Instructions

- Quality rating 01 the Illustrations

- Is this 58 easy to understand?

4 3

4 3

4 3

Y/N

2

2

2

If you 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 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"identitication X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator:

NamefTitle:

Please return this form to.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rend Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Atln SEM4 Service Bulletins Management

FAX (33) 5 61 934251

Or via 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.