~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 (i AIRBUS SAS. 2007. All rights reserved.
EFFECTIVITY

This Service Bulletin is applicable 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 OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 250486-831-801-001: Modilication

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) I 2.00

PEN0 ICES

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

REVISION No.: 00 - Sep 21/09 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

REVISION No: 00 - Sep 21/09 Page: 4
SERVICE BUL~ETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEOEX

FRANCE

Tei: (33) 5 61 93 33 33

Telex: AIRBU 530526F

Fax. (33) 5 61 934251

ATA SYSTEM: 25

TITLE: EQUIPMENT I FURNISHINGS· COCKPIT· DOOR MODULE

IMPROVEMENT

MODIFICATION No,: 13545023270

This document conlains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property 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 ~xpress condition that said document and the

information contained in it shall be treated as confidenti~l, 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 10third 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

dCONF ALL

A. EFFECTIVITY

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

intrusion and penetration resistant cockpit door is installed.

(1) Models

82-203 B2K-3C B4-103 84-120' 84-203 B4-2C

(2) Effectivity by MSN

00550079-008000820090009401280,1330135-01380151 015601600170

0175-01760180 0185 0187 0190 0192 O~040226 0239 0243-0244 0256 0299 0302

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance wah the informdtion available to AIRBUS. Any future changes

resulting from transfer of an aircraft froml one operator to another will not be reflected in

this list unless the Service Bulletin is revised lor another reason.

5

OP61t1llt"/!,

AFG

F21

FLM

DATE: Sep 21/09

01800190 I

0079 0094 0128 0133 0135 0136 0137 0156 0170 0243

0082015101760256

I

SERVICE BULLETIN No.. A300-25-0486

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

Printed in FRANCE to AIRBUS 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~ on the door frame.

(3) Advantages

Accomplishment of this serce Bulletin will 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 of the 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. EASA 21J.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

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

included.

Get Access 0.50

On Aircraft

Install the Springs on the Strike of the 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

Not Changed

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

L. INTERCHANG EABILITY /MIXAJILITY

K.

Not Applicable

M. SPARES

None

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486

REVISION No: 00 - Sep 21/09 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 is the subject of an AIRBUS monitored retrofit campaign.

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

For ordering by fax: +49.40.50.76.25.90

No AIRBUS kit will be provided.

Parts required to accomplish this servici Bulletin can be manufactured by the operator

following the Fig. A-FBBAA Sheet 01 or ordered by a spare purchase order 10AIRBUS

B. INDUSTRY SUPPORT INFORMATION

For the 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) 5 61 932745

Parts are at 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.. A300-25-0486

REVISION No.: 00 - Sep 21/09 Page: 5
I~A300

SERVICE BULLETIN

D. LIST OF MATERIALS· OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLAOl

ITEM DESCRIPTION I

REFERENCE TO CML QTY PER Ale 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. PARTS TO BE HE-iDENTIFIED BY OPERATOR

None

F. TOOLING

None

5 DATE: Sep 21109 SEAVICE BULLETIN No.: A300-25-0486

REVISION No.: 00 - Sep 21109 Page: 6

Printed in FRANCE e AIRBUS 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 IN THE 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 do the job

, - -

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 Repair Manual (SRM) 51-30-29

(a) For the specification of the material numbers (Mat. No.), refer to Consumable

Material List (CML).

As required

Skills

I

NON SPECIFIC

in this

8. PREPARATION

I

I

I

AIRFRAME

I

I

I

:~'·J:~,er\W~es0u.rpe'S

I

I

(1) Sublask 250486-941-001-0,01 - Job Set-up

I I

<*'. ",;LJ,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 sure that the a'reraft is electrically grout')ded (Reier to AMM 24-00-00, Page

Block 301).

(b) Put access platform in position

I

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

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486

REVISION No: 00· Sep 21/09 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 10 do 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 QTY PER Ale

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

Printed in 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 on the door the !AdhesIVetape on all surface In contact between the door and

the springs Item 1 I

Adhesive tape DAN269-25 1 {M}

D. TEST

-

Door 831

,<J~erR~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

AircraftMaintenanceManual(AM~) 52-5H 1, PageBlock501

I

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

- If the door is IOU~dhard to open (or close!), do the adjustment of the 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 Block 001

(a) Make sure that the fork areas are clean and clear of tools and other items of

equipment. I

(b) Close the 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 of the 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}

Figure A-FBAAA - Sheet 02

Instaliation of Springs on the Strike of the Cockpit Door

5 DATE: Sep 21/09 SERVICE BULLETIN No.: A300-25-0486

REVISION No.: 00 - Sep 21109 Page: 12

Printed in FRANCE C AIRBUS SAS. 2007. All rights resewed.
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 of the Cockpit Door

SERVICE BULLETIN No.: A300-25-0486

REVISION No.: 00 - Sep 21109 Page: 13

Printed in FRANCE e AIRBUS S.A.S. 2007. All rights reserved_
'$;A300

SERVICE BULLETIN

"CONF ALL

PRINCIPLE OF MANUFACTURE

10 mm

10.394 In)

l.gmm Ai (0.075 in)

R.Wmm

(0.384 ;n)

DIAM.

(0,390

9,91 mm

In),

I

I

1

, .

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..229 In)

A-A

:m.2 mm

(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-lE SPRING WITli PART

NUMBER'1a3357

NOTE,

NOT SPECIFIED RADIUS; R. 3 mtn (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

REVISION No,' 0.0- Sep 21/09 Pags: 14

Prin'oo In FflANC~ © AIRBUS SAS. 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 - Sep 21/09 Page: 1

Printed in FRANCE iD AIRBUS 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 BE embodied YES/NO(if NO please 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 10 S8 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 e AIRBUS S.A.S. 2007. All rigllls reserved.
~A300

SERVICE BULLETIN

QUALITY PERCEPi'ON FORM

Use this form 10 tell us what is your perception of the quality 01 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. 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 of this S8

- Quality rating of the Accomplishment Instructions

- Quality rating of the Illustrations

- Is this S8 easy to understand?

4 3

4 3

4 3

Y/N

2

2

2

If you have had difficulties in the accomplishment of this 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 this torm toAIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellante

31707 BLAGNAC CEDEX FRANCE

Atln : 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.: A300-25-0486

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

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