@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 52

TITLE: DOORS - CARGO DOORS - INSPECTION OF FWD AND AFT CARGO

DOORS FOR NON CONFORMITY

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Investigations have shown that an identified batch of cargo doors might have deviations in quality, such

as irregular bore holes, improper application of sealant and paint or cleanliness. These deviations are

related to the quality of the door structure. AIRBUS have decided to inspect the in-service aircraft with

potentially affected forward (FWD) and aft (AFT) cargo doors delivered since end of 2006.

This Service Bulletin details the procedure to inspect the cargo doors for non-conformity of the cargo

doors structure with the specification requirements. Non-conformity will lead to the replacement of the

cargo doors.

The accomplishment of this Service Bulletin ensures the conformity of the cargo door structure with the

specification requirements.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

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SERVICE BULLETIN

SUMMARY

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

46W 97X AAR AAW AFL ARA AVA CAL CCA CES CHH CPA CSC

CSN DAL DLH EIN ETD FIN GFA GIA HVN JAI JST KFR MEA

OMA QFA QTR SIA SWR TAM TAP THA TSC UAF USA XAX

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER OIT 999.0016/10

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 523083-832-848-001: Inspection

TOTAL MANHOURS 0.75

ELAPSED TIME (HOURS) 0.75

**CONF 002

Task 523083-832-848-001: Inspection

TOTAL MANHOURS 0.75

ELAPSED TIME (HOURS) 0.75

**CONF 003

Task 523083-832-848-001: Inspection

TOTAL MANHOURS 1.25

ELAPSED TIME (HOURS) 1.25

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

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SERVICE BULLETIN

SUMMARY

APPENDICES

**CONF ALL

None

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SERVICE BULLETIN

SUMMARY

**CONF ALL

FR26

FR20

FR65

FR59A

A

B

SERIAL NUMBER TO BE INSPECTED

SERIAL NUMBER TO BE INSPECTED

Z132

Z152

A

B

PART NUMBER AND

PART NUMBER AND

G_SB_523083_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 52

TITLE: DOORS - CARGO DOORS - INSPECTION OF FWD AND AFT CARGO

DOORS FOR NON CONFORMITY

MODIFICATION No.: None

This document contains 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 express condition that said document and the

information contained in it shall be treated as confidential, 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 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

**CONF ALL

A. EFFECTIVITY

(1) Models

330-202 330-203 330-223 330-243 330-302 330-323 330-342 330-343

(2) Effectivity by MSN

0796 0832 0840 0845 0849 0853 0855 0861-0862 0866 0868 0871 0873 0876 0879

0882 0885 0887 0889 0891-0892 0896 0898-0899 0903-0905 0907 0913 0927 0930

0935-0937 0940 0943-0944 0946 0949 0952 0954 0964 0971 0975 0982-0986

0988-0990 0992 0994-0995 0997-0999 1001-1003 1006-1007 1009-1016 1018 1020

1022-1023 1026 1028-1029 1037 1045 1049 1052-1053 1055 1058 1060-1061

1065-1067 1071-1075 1077 1080 1082

(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.

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SERVICE BULLETIN

OPERATOR MSN

46W 0871

97X 1053

AAR 0845 1001 1055

AAW 0999

AFL 1014 1045 1058 1065 1072 1077

ARA 1002

AVA 1009 1016 1073

CAL 0861

CCA 0873 0903 0930 0944

CES 0862 0866 0936

CHH 0982

CPA 0855

CSC 1082

CSN 0840 0879 0889 0935 0937 0954 0964

DAL 0796

DLH 0896 0905 0913 0989

EIN 0985

ETD 0832 0868 0975 1071

FIN 0994 1007 1013 1023 1067

GFA 0992

GIA 0988 1020 1028 1052

HVN 0943

JAI 0882 0885

JST 0853 0940

KFR 0891 0927 0946

MEA 0984 0995 0998

OMA 1049

QFA 0887 0892 0898 1061

QTR 0849 0907

SIA 0983 0986 0997 1006 1010 1012 1015

SWR 1018 1026 1029

TAM 0876 0949

TAP 0899 0904

THA 0990 1003 1037 1060 1074

TSC 0971

UAF 1080

USA 1011 1022

XAX 0952 1066 1075

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0796 0840 0845 0849 0853 0855 0861 0862 0866 0868 0871

0873 0876 0879 0882 0885 0887 0889 0891 0892 0896 0898

0899 0903 0904 0905 0907 0913 0935 0936 0937 0940 0943

0944 0946 0949 0954 0964 0971 0975 0982 0983 0984 0985

0986 0988 0989 0990 0992 0994 0995 0997 0998 0999 1001

1002 1003 1006 1007 1009 1010 1014 1015 1018 1022 1028

1029 1037 1045 1055 1060 1061 1067 1071 1072 1073 1075

001

0832 0927 0930 0952 1011 1016 1049 1052 002

1012 1013 1020 1023 1026 1053 1058 1065 1066 1074 1077

1080 1082

003

(5) Configuration definition

**CONF 001

Config. 001 is valid for all aircraft where only the FWD cargo door must be inspected.

**CONF 002

Config. 002 is valid for all aircraft where only the AFT cargo door must be inspected.

**CONF 003

Config. 003 is valid for all aircraft where the FWD and AFT cargo door must be

inspected.

(6) Material Effectivity

No Material Set

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Investigations have shown that an identified batch of cargo doors might have deviations

in quality, such as irregular bore holes, improper application of sealant and paint or

cleanliness. These deviations are related to the quality of the door structure. AIRBUS

have decided to inspect the in-service aircraft with potentially affected forward (FWD)

and aft (AFT) cargo doors delivered since end of 2006.

(2) Objective/Action

This Service Bulletin details the procedure to inspect the cargo doors for non-conformity

of the cargo doors structure with the specification requirements. Non-conformity will lead

to the replacement of the cargo doors.

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SERVICE BULLETIN

(3) Advantages

The accomplishment of this Service Bulletin ensures the conformity of the cargo door

structure with the specification requirements.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 523083-832-848-001: Inspection

(1) Inspect the FWD cargo door for non-conformity of the cargo door structure with the

specification requirements

**CONF 002

Task 523083-832-848-001: Inspection

(1) Inspect the AFT cargo door for non-conformity of the cargo door structure with the

specification requirements

**CONF 003

Task 523083-832-848-001: Inspection

(1) Inspect the FWD and AFT cargo door for non-conformity of the cargo door structure

with the specification requirements

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the thresholds

given below but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

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SERVICE BULLETIN

Table 1, Config. 001 - FWD cargo door general visual inspection for non-conformity of the cargo door

structure with the specification requirements

Condition Action Compliance time

(Whichever occurs first)

All aircraft Identify the Part Number (PN)

and the Serial Number (SN) on

the identification plate of the

FWD cargo door

Within 7400 FC

OR

within 6 years

from aircraft first flight

All aircraft Compare the PN and SN with

the list of affected PN and SN

given in this Service Bulletin

Within 7400 FC

OR

within 6 years

from aircraft first flight

Cargo door affected Replace the cargo door with a

serviceable door

Within 7400 FC

OR

within 6 years

from aircraft first flight

Cargo door not affected Contact AIRBUS and follow their

instructions

Within 3 months from the

inspection

**CONF 002

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the thresholds

given below but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

Table 2, Config. 002 - AFT cargo door general visual inspection for non-conformity of the cargo door

structure with the specification requirements

Condition Action Compliance time

(Whichever occurs first)

All aircraft Identify the Part Number (PN)

and the Serial Number (SN) on

the identification plate of the AFT

cargo door

Within 7400 FC

OR

within 6 years

from aircraft first flight

All aircraft Compare the PN and SN with

the list of affected PN and SN

given in this Service Bulletin

Within 7400 FC

OR

within 6 years

from aircraft first flight

Cargo door affected Replace the cargo door with a

serviceable door

Within 7400 FC

OR

within 6 years

from aircraft first flight

Cargo door not affected Contact AIRBUS and follow their

instructions

Within 3 months from the

inspection

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

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SERVICE BULLETIN

**CONF 003

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the thresholds

given below but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

Table 3, Config. 003 - FWD and AFT cargo door general visual inspection for non-conformity of the

cargo door structure with the specification requirements

Condition Action Compliance time

(Whichever occurs first)

All aircraft Identify the Part Number (PN)

and the Serial Number (SN) on

the identification plate of the

FWD and AFT cargo door

Within 7400 FC

OR

within 6 years

from aircraft first flight

All aircraft Compare the PN and SN with

the list of affected PN and SN

given in this Service Bulletin

Within 7400 FC

OR

within 6 years

from aircraft first flight

Cargo door affected Replace the cargo door with a

serviceable door

Within 7400 FC

OR

within 6 years

from aircraft first flight

Cargo door not affected Contact AIRBUS and follow their

instructions

Within 3 months from the

inspection

**CONF ALL

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organisation Approval No. EASA.21J.031.

If 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 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 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 of parts

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

included.

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

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SERVICE BULLETIN

**CONF 001

Task 523083-832-848-001: Inspection

Get Access 0.25

On Aircraft

Inspect the FWD cargo door for non-conformity of the

cargo door structure with the specification requirements

0.25

Close-Up 0.25

TOTAL MANHOURS 0.75

ELAPSED TIME (HOURS) 0.75

**CONF 002

Task 523083-832-848-001: Inspection

Get Access 0.25

On Aircraft

Inspect the AFT cargo door for non-conformity of the

cargo door structure with the specification requirements

0.25

Close-Up 0.25

TOTAL MANHOURS 0.75

ELAPSED TIME (HOURS) 0.75

**CONF 003

Task 523083-832-848-001: Inspection

Get Access 0.50

On Aircraft

Inspect the FWD and AFT cargo door for nonconformity of the cargo door structure with the

specification requirements

0.25

Close-Up 0.50

TOTAL MANHOURS 1.25

ELAPSED TIME (HOURS) 1.25

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

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SERVICE BULLETIN

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 12-34-24 52-31-11 52-36-00

Elec. Std. Practices Manual (ESPM) 20-55-00

**CONF 002

Aircraft Maintenance Manual (AMM) 12-34-24 52-32-11 52-36-00

Elec. Std. Practices Manual (ESPM) 20-55-00

**CONF 003

Aircraft Maintenance Manual (AMM) 12-34-24 52-31-11 52-32-11

52-36-00

Elec. Std. Practices Manual (ESPM) 20-55-00

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet: http://spares.airbus.com

For ordering modification kits by fax: +49 40 50 76 25 90

For ordering of single spares by fax: +49 40 50 76 40 12

(2) Price and Availability

No AIRBUS kit will be provided. Parts required to accomplish this Service Bulletin are to

be purchased by a Spares Purchase Order.

B. INDUSTRY SUPPORT INFORMATION

Affected cargo doors whose part numbers and serial numbers are listed in this Service

Bulletin, AIRBUS will provide the replacement doors at no charge, and will credit the

manhours for the correction at the agreed in-house warranty labor rate. Claims for

reimbursement of door painting costs will also be accepted. All claims should be sent not later

than 90 days after completion of the last affected aircraft of your fleet.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 523083-832-848-001 - Inspection

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.75

ELAPSED TIME (HOURS) 0.75

**CONF 002

Manpower

TOTAL MANHOURS 0.75

ELAPSED TIME (HOURS) 0.75

**CONF 003

Manpower

TOTAL MANHOURS 1.25

ELAPSED TIME (HOURS) 1.25

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**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 523083-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

(a) The purpose of flow charts are for information only to show the various

Inspection/Repair phases described in this Service Bulletin.

(2) Subtask 523083-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 523083-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

(a) The purpose of flow charts are for information only to show the various

Inspection/Repair phases described in this Service Bulletin.

(2) Subtask 523083-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 003

(1) Subtask 523083-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

(a) The purpose of flow charts are for information only to show the various

Inspection/Repair phases described in this Service Bulletin.

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SERVICE BULLETIN

(2) Subtask 523083-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 523083-941-202-003 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

52-36-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position at the FWD cargo door.

(c) Open the FWD cargo door (Refer to AMM 52-36-00, Page Block 001).

**CONF 002

(1) Subtask 523083-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

52-36-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position at the AFT cargo door.

(c) Open the AFT cargo door (Refer to AMM 52-36-00, Page Block 001).

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SERVICE BULLETIN

**CONF 003

(1) Subtask 523083-941-202-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

52-36-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platforms in position at the FWD and AFT cargo doors.

(c) Open the FWD and AFT cargo doors (Refer to AMM 52-36-00, Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 523083-832-201-002 - Inspect the FWD cargo door for non-conformity of

the cargo door structure with the specification requirements

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-31-11, Page Block 401

Fig. A-GBAAA

Cargo door PN and SN identification

Sheet 01 - Identification plate location

Sheet 02 - Cargo door PN and SN reference

list

Sheet 03 - Cargo door PN and SN reference

list

Fig. A-GFAAA

Flow Chart

Sheet 01

Fig. A-GRAAB

Report sheet

Sheet 01

(a) On the FWD cargo door, identify the cargo door PN and SN as given in the Flow

Chart Fig. A-GFAAA Sheet 01 and as shown on Fig. A-GBAAA Sheet 01.

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(b) Compare the cargo door PN and SN with the reference list Fig. A-GBAAA Sheet 02

and Fig. A-GBAAA Sheet 03.

1 If the cargo door is affected in accordance with the reference list, replace the

cargo door with a serviceable door (Refer to AMM 52-31-11, Page Block 401).

NOTE: A serviceable cargo door is a door which is not listed in the

reference list Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03.

2 If the cargo door is not affected, contact AIRBUS and follow their instructions.

Use the report sheet Fig. A-GRAAB Sheet 01.

**CONF 002

(1) Subtask 523083-832-202-002 - Inspect the AFT cargo door for non-conformity of

the cargo door structure with the specification requirements

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-32-11, Page Block 401

Fig. A-GBAAA

Cargo door PN and SN identification

Sheet 01 - Identification plate location

Sheet 02 - Cargo door PN and SN reference

list

Sheet 03 - Cargo door PN and SN reference

list

Fig. A-GFAAA

Flow Chart

Sheet 01

Fig. A-GRAAC

Report sheet

Sheet 01

(a) On the AFT cargo door, identify the cargo door PN and SN as given in the Flow

Chart Fig. A-GFAAA Sheet 01 and as shown on Fig. A-GBAAA Sheet 01.

(b) Compare the cargo door PN and SN with the reference list Fig. A-GBAAA Sheet 02

and Fig. A-GBAAA Sheet 03.

1 If the cargo door is affected in accordance with the reference list, replace the

cargo door with a serviceable door (Refer to AMM 52-32-11, Page Block 401).

NOTE: A serviceable cargo door is a door which is not listed in the

reference list Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03.

2 If the cargo door is not affected, contact AIRBUS and follow their instructions.

Use the report sheet Fig. A-GRAAC Sheet 01.

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 15

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SERVICE BULLETIN

**CONF 003

(1) Subtask 523083-832-203-002 - Inspect the FWD and AFT cargo door for nonconformity of the cargo door structure with the specification requirements

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-31-11, Page Block 401

52-32-11, Page Block 401

Fig. A-GBAAA

Cargo door PN and SN identification

Sheet 01 - Identification plate location

Sheet 02 - Cargo door PN and SN reference

list

Sheet 03 - Cargo door PN and SN reference

list

Fig. A-GFAAA

Flow Chart

Sheet 01

Fig. A-GRAAA

Report sheet

Sheet 01

(a) On the FWD and AFT cargo door, identify the cargo door PN and SN as given in

the Flow Chart Fig. A-GFAAA Sheet 01 and as shown on Fig. A-GBAAA Sheet 01.

(b) Compare the cargo door PN and SN with the reference list Fig. A-GBAAA Sheet 02

and Fig. A-GBAAA Sheet 03.

1 If the FWD and/or AFT cargo door is affected in accordance with the reference

list, replace the affected cargo door with a serviceable door (Refer to AMM

52-31-11, Page Block 401 for the FWD cargo door and refer to AMM

52-32-11, Page Block 401 for the AFT cargo door).

NOTE: A serviceable cargo door is a door which is not listed in the

reference list Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03.

2 If the FWD and/or AFT cargo door is not affected, contact AIRBUS and follow

their instructions. Use the report sheet Fig. A-GRAAA Sheet 01.

**CONF ALL

D. TEST

**CONF 001

None

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 16

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SERVICE BULLETIN

**CONF 002

None

**CONF 003

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 523083-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-36-00, Page Block 001

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

equipment.

(b) Close the FWD cargo door (Refer to AMM 52-36-00, Page Block 001).

(c) Remove the access platform(s) from the FWD cargo door.

**CONF 002

(1) Subtask 523083-942-201-003 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-36-00, Page Block 001

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

equipment.

(b) Close the AFT cargo door (Refer to AMM 52-36-00, Page Block 001).

(c) Remove the access platform(s) from the AFT cargo door.

**CONF 003

(1) Subtask 523083-942-201-004 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 17

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 52-36-00, Page Block 001

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

equipment.

(b) Close the FWD and AFT cargo doors (Refer to AMM 52-36-00, Page Block 001).

(c) Remove the access platforms from the FWD and AFT cargo doors.

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 18

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@A330

SERVICE BULLETIN

**CONF ALL

A/C

MFR PN

DESCR.

SER. N°

MFG DATE

Z132

Z152

FR26

FR20

FR65

FR59A

A

B

A

B

C

C

UHXXXX

PART NUMBER TO BE INSPECTED

C

NOTE:

01 FOR THE AFFECTED PART NUMBERS AND SERIAL NUMBERS

01

REFER TO REFERENCE LIST ON SHEETS 2 AND 3. G_SB_523083_6_BAAA_01_02

F523−70550−XXX−00

01 SERIAL NUMBER 

TO BE INSPECTED

Figure A-GBAAA - Sheet 01

Cargo door PN and SN identification - Identification plate location

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 19

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@A330

SERVICE BULLETIN

**CONF ALL

796 F523−70550−116−00 UH1794

832 F523−72300−106−00 UH1830

840 F523−70550−116−00 UH1838

845 F523−70550−116−00 UH1843

849 F523−70550−116−00 UH1847

853 F523−70550−116−00 UH1851

855 F523−70550−116−00 UH1853

861 F523−70550−116−00 UH1859

862 F523−70550−116−00 UH1860

866 F523−70550−116−00 UH1864

868 F523−70550−116−00 UH1866

871 F523−70550−116−00 UH1869

873 F523−70550−116−00 UH1906

876 F523−70550−116−00 UH1874

879 F523−70550−116−00 UH1877

882 F523−70550−116−00 UH1880

887 F523−70550−116−00

UH1882

889 F523−70550−116−00

UH1885

891 F523−70550−116−00

UH1887

892 F523−70550−116−00

UH1889

896 F523−70550−116−00

UH1890

898 F523−70550−116−00

UH1894

899 F523−70550−116−00

UH1896

903 F523−70550−116−00

UH1898

904 F523−70550−116−00

UH1901

905 F523−70550−116−00

UH1902

907 F523−70550−116−00

UH1903

913 F523−70550−116−00

UH1905

927 F523−72300−108−00 UH1925

930 F523−72300−108−00 UH1928

935 F523−70550−116−00 UH1933

936 F523−70550−116−00 UH1934

937 F523−70550−116−00 UH1935

940 F523−70550−116−00 UH1938

943 F523−70550−116−00 UH1941

944 F523−70550−116−00 UH1942

946 F523−70550−116−00 UH1944

949 F523−70550−116−00 UH1947

952 F523−72300−110−00 UH1950

954 F523−70550−116−00 UH1952

964 F523−70550−118−00 UH1962

971 F523−70550−118−00 UH1969

975 F523−70550−118−00 UH1973

982 F523−70550−118−00 UH1980

983 F523−70550−118−00 UH1981

984 F523−70550−118−00 UH1982

985 F523−70550−118−00 UH1983

MSN Forward P/N Aft P/N Forward S/N Aft S/N

885 F523−70550−116−00

UH1871

G_SB_523083_6_BAAA_02_04

Figure A-GBAAA - Sheet 02

Cargo door PN and SN identification - Cargo door PN and SN reference list

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 20

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SERVICE BULLETIN

**CONF ALL

988 F523−70550−118−00 UH1986

989 F523−70550−118−00 UH1987

990 F523−70550−118−00 UH1988

992 F523−70550−118−00 UH1990

994 F523−70550−118−00 UH1992

995 F523−70550−118−00 UH1993

997 F523−70550−120−00 UH1995

998 F523−70550−118−00 UH1996

999 F523−70550−120−00 UH1997

1001 F523−70550−120−00 UH1999

1002 F523−70550−120−00 UH2000

1003 F523−70550−120−00 UH2001

1006 F523−70550−120−00 UH2004

1007 F523−70550−120−00 UH2005

1010 F523−70550−120−00 UH2008

1011 F523−72300−114−00 UH2009

1012 F523−70550−120−00 F523−72300−112−00 UH2010* UH2010*

1013 F523−70550−120−00 F523−72300−112−00 UH2011* UH2011*

1014 F523−70550−120−00 UH2012

1015 F523−70550−120−00 UH2013

1016 F523−72300−112−00 UH2014

1018 F523−70550−120−00 UH2016

1020 F523−70550−120−00 F523−72300−112−00 UH2018* UH2018*

1022 F523−70550−122−00 UH2020

1023 F523−70550−120−00 F523−72300−112−00 UH2021* UH2021*

1026 F523−70550−120−00 F523−72300−112−00 UH2024* UH2024*

1028 F523−70550−120−00 UH2026

1029 F523−70550−120−00 UH2027

1037 F523−70550−122−00 UH2035

1045 F523−70550−122−00 UH2042

1049 F523−72300−114−00 UH62023

1052 F523−72300−114−00 UH62021

1053 F523−70550−122−00 F523−72300−114−00 UH61079 UH62022

1055 F523−70550−122−00 UH2053

1058 F523−70550−122−00 F523−72300−114−00 UH61090 UH62025

1060 F523−70550−122−00 UH61092

1061 F523−70550−122−00 UH61093

1065 F523−70550−122−00 F523−72300−114−00 UH61094 UH62014

1066 F523−70550−122−00 F523−72300−114−00 UH61095 UH62026

1067 F523−70550−122−00 UH61097

1071 F523−70550−122−00 UH61096

1072 F523−70550−122−00 UH61099

1073 F523−70550−122−00 UH61080

1074 F523−70550−122−00 F523−72300−114−00 UH61081 UH62028

1075 F523−70550−122−00 UH61082

1077 F523−70550−122−00 F523−72300−114−00 UH61078 UH62029

1080 F523−70550−122−00 F523−72300−114−00 UH61083 UH62030

1082 F523−70550−122−00 F523−72300−114−00 UH61084 UH62031

MSN Forward P/N Aft P/N Forward S/N Aft S/N

986 F523−70550−118−00 UH1984

1009 F523−70550−120−00 UH2007

* SAME S/N, BUT FOR DIFFERENT P/N G_SB_523083_6_BAAA_03_02

Figure A-GBAAA - Sheet 03

Cargo door PN and SN identification - Cargo door PN and SN reference list

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 21

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@A330

SERVICE BULLETIN

**CONF ALL

IDENTIFY THE 

CARGO DOOR P/N AND S/N

NO YES

DOOR AFFECTED

IN ACCORDANCE WITH

CARGO

THE REFERENCE

NO FURTHER ACTION NECESSARY

IN ACCORDANCE WITH THIS

SERVICE BULLETIN

COMPARE THE P/N AND S/N

WITH THE REFERENCE LIST

LIST

REPLACE THE AFFECTED 

THE REPORT SHEET TO AIRBUS CARGO DOOR

COMPLETE AND SEND

G_SB_523083_6_FAAA_01_04

Figure A-GFAAA - Sheet 01

Flow Chart

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 22

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@A330

SERVICE BULLETIN

**CONF 003

REPORT SHEET

SERVICE BULLETIN NO:

DATE OF INSPECTION:

A/C MSN:

FLIGHT CYCLES:

FLIGHT HOURS:

CARGO DOORS

A330−52−3083

AIRBUS DEPARTMENT SEES3

CUSTOMER SERVICE ENGINEERING 

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

Please send reporting sheet to:

YES NO

FAX +33 (0)5 61 93 36 14

FWD

CARGO DOOR

AFT

CARGO DOOR

CARGO DOOR AFFECTED

(IN ACCORDANCE WITH 

SERIAL NUMBER

YES NO

SERIAL NUMBER

THE REFERENCE LIST)

DATE OF REPLACEMENT

REMARKS:

REPLACEMENT

PART NUMBER PART NUMBER

G_SB_523083_6_RAAA_01_03

Figure A-GRAAA - Sheet 01

Report sheet

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 23

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@A330

SERVICE BULLETIN

**CONF 001

REPORT SHEET

SERVICE BULLETIN NO:

DATE OF INSPECTION:

A/C MSN:

FLIGHT CYCLES:

FLIGHT HOURS:

CARGO DOORS

A330−52−3083

AIRBUS DEPARTMENT SEES3

CUSTOMER SERVICE ENGINEERING 

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

Please send reporting sheet to:

FAX +33 (0)5 61 93 36 14

FWD

CARGO DOOR

CARGO DOOR AFFECTED

(IN ACCORDANCE WITH YES NO

THE REFERENCE LIST)

REPLACEMENT

G_SB_523083_6_RAAB_01_01

SERIAL NUMBER

DATE OF REPLACEMENT

REMARKS:

PART NUMBER

Figure A-GRAAB - Sheet 01

Report sheet

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 24

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@A330

SERVICE BULLETIN

**CONF 002

REPORT SHEET

SERVICE BULLETIN NO:

DATE OF INSPECTION:

A/C MSN:

FLIGHT CYCLES:

FLIGHT HOURS:

CARGO DOORS

A330−52−3083

AIRBUS DEPARTMENT SEES3

CUSTOMER SERVICE ENGINEERING 

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

Please send reporting sheet to:

FAX +33 (0)5 61 93 36 14

AFT

CARGO DOOR

CARGO DOOR AFFECTED

(IN ACCORDANCE WITH YES NO

THE REFERENCE LIST)

REPLACEMENT

G_SB_523083_6_RAAC_01_01

SERIAL NUMBER

DATE OF REPLACEMENT

REMARKS:

PART NUMBER

Figure A-GRAAC - Sheet 01

Report sheet

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 25

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@A330

SERVICE BULLETIN

REPORTING SHEET

TITLE: DOORS - CARGO DOORS - INSPECTION OF FWD AND AFT CARGO

DOORS FOR NON CONFORMITY

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

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

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision 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 operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 1

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@A330

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 SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB 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: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: May 31/11 SERVICE BULLETIN No.: A330-52-3083

REVISION No.: 00 - May 31/11 Page: 1

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