@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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: 54

TITLE: NACELLES/PYLON - INSPECT PYLON LOWER SPAR BETWEEN RIBS

9 AND 10

MODIFICATION No.: None

This page transmits Revision No.03 of Service Bulletin No.A300-54-6011

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 03 issued to inform operators that revised inspection thresholds, repeat intervals and

grace periods have been introduced to support aircraft operations to Extended Service Goal 2 (ESG2).

CHANGES

SUMMARY

MODIFICATIONS Minor editorial or document structure change N

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

Minor editorial or document structure change N

GENERAL EVALUATION Minor editorial or document structure change N

MATERIAL PRICE INFORMATION Minor editorial or document structure change N

Minor editorial or document structure change N

EFFECTIVITY Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REFERENCES / REPERCUSSIONS Minor editorial or document structure change N

NATURE OF THE WORK Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

APPENDICES Minor editorial or document structure change N

Fig. A-FSAAA Minor editorial or document structure change N

Fig. A-FSAAA Sheet 01 Minor editorial or document structure change N

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 1

5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

PLANNING INFORMATION

EFFECTIVITY Minor editorial or document structure change N

Configuration definition Minor editorial or document structure change N

CONF 001 Minor editorial or document structure change N

CONF 002 Minor editorial or document structure change N

Material Effectivity Minor editorial or document structure change N

Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REASON Minor editorial or document structure change N

History Minor editorial or document structure change N

Objective/Action Minor editorial or document structure change N

Advantages Minor editorial or document structure change N

Operational/Maintenance

Consequences

Minor editorial or document structure change N

DESCRIPTION Minor editorial or document structure change N

COMPLIANCE Minor editorial or document structure change N

Classification Minor editorial or document structure change N

Accomplishment Timescale Minor editorial or document structure change N

APPROVAL Minor editorial or document structure change N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

WEIGHT AND BALANCE Minor editorial or document structure change N

ELECTRICAL LOAD DATA Minor editorial or document structure change N

REFERENCES Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

PUBLICATION AFFECTED Minor editorial or document structure change N

INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N

SPARES Minor editorial or document structure change N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N

Procurement Addresses Minor editorial or document structure change N

Price and Availability Minor editorial or document structure change N

INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N

LIST OF COMPONENTS Minor editorial or document structure change N

Kit 546011A01R03 Minor editorial or document structure change N

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change N

Consumable Materials Minor editorial or document structure change N

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Consumable CMLA01 Minor editorial or document structure change N

Components Minor editorial or document structure change N

Equipment Minor editorial or document structure change N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

Minor editorial or document structure change N

TOOLING Minor editorial or document structure change N

Tooling - Price and Availability Minor editorial or document structure change N

Tools Minor editorial or document structure change N

Special Tools Minor editorial or document structure change N

ACCOMPLISHMENT INSTRUCTIONS

TASK 546011- 832-801-001-Inspection Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N

Task associated data - 002 Minor editorial or document structure change N

Subtask 546011-839-001-001 Minor editorial or document structure change N

Subtask 546011-839-001-001 Minor editorial or document structure change N

Subtask 546011-941-001-001 Minor editorial or document structure change N

Subtask 546011-941-001-002 Minor editorial or document structure change N

Subtask 546011-832-001-001 Minor editorial or document structure change N

Subtask 546011-832-002-001 Minor editorial or document structure change N

Subtask 546011-832-003-001 Minor editorial or document structure change N

Subtask 546011-832-004-001 Minor editorial or document structure change N

Subtask 546011-832-005-001 Minor editorial or document structure change N

Subtask 546011-832-006-001 Minor editorial or document structure change N

Subtask 546011-832-001-001 Minor editorial or document structure change N

Subtask 546011-832-002-001 Minor editorial or document structure change N

Subtask 546011-832-003-001 Minor editorial or document structure change N

Subtask 546011-832-004-001 Minor editorial or document structure change N

Subtask 546011-832-005-001 Minor editorial or document structure change N

Subtask 546011-832-006-001 Minor editorial or document structure change N

Subtask 546011-942-001-001 Minor editorial or document structure change N

Subtask 546011-942-001-002 Minor editorial or document structure change N

TASK 546011- 833-801-001-Repair Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N

Task associated data - 002 Minor editorial or document structure change N

Subtask 546011-910-001-001 Minor editorial or document structure change N

Subtask 546011-839-002-001 Minor editorial or document structure change N

Subtask 546011-910-001-001 Minor editorial or document structure change N

Subtask 546011-839-002-001 Minor editorial or document structure change N

Subtask 546011-941-003-001 Minor editorial or document structure change N

Subtask 546011-941-003-001 Minor editorial or document structure change N

Subtask 546011-833-001-001 Minor editorial or document structure change N

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 546011-833-002-001 Minor editorial or document structure change N

Subtask 546011-833-001-001 Minor editorial or document structure change N

Subtask 546011-833-002-001 Minor editorial or document structure change N

Subtask 546011-700-002-001 Minor editorial or document structure change N

Subtask 546011-700-002-001 Minor editorial or document structure change N

Subtask 546011-942-002-001 Minor editorial or document structure change N

Subtask 546011-942-002-001 Minor editorial or document structure change N

Fig. A-FBAAA Minor editorial or document structure change N

Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FBBAA Minor editorial or document structure change N

Fig. A-FBBAA Sheet 01 Minor editorial or document structure change N

Fig. A-FBCAA Minor editorial or document structure change N

Fig. A-FBCAA Sheet 01 Minor editorial or document structure change N

Fig. A-FFAAA Minor editorial or document structure change N

Fig. A-FFAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FFAAA Sheet 02 Minor editorial or document structure change N

Fig. A-FFAAA Sheet 03 Minor editorial or document structure change N

APPENDIX 01

APPENDIX CONTENT Minor editorial or document structure change N

Fig. A-FRAAA Minor editorial or document structure change N

Fig. A-FRAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FRAAA Sheet 02 Minor editorial or document structure change N

Fig. A-FRAAA Sheet 03 Minor editorial or document structure change N

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision No.01 issued to add an inspection program after accomplishment of the Service Bulletin No.

A300-54-6019 (Mod. No. 10328S20412).

Revision No.02 issued to add the liquid penetrant inspection (Refer to NTM 54-50-40, Part 9) as an

alternative to Eddy current inspection (Refer to NTM 54-50-40, Part 6) and to incorporate Change

Notice No. 1.A., 1.B., 1.C.

REVISION SEQUENCE

ORIGINAL: Nov 12/91

REVISION No.: 01 - Oct 15/93

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 4

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@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION No.: 02 - Aug 25/00

REVISION No. : 03 - Jun 23/11

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 5

5

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@A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 6

5

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@A300-600

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: 54

TITLE: NACELLES/PYLON - INSPECT PYLON LOWER SPAR BETWEEN RIBS

9 AND 10

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

On aircraft fitted with Pratt and Whitney pylon, crack has been reported on pylon lower spar.

The crack is running between ribs 9 and 10 and is starting on the center stiffener after the flat area.

The aim of this Service Bulletin is to call for eddy current or liquid penetrant inspection of the pylon

lower spar in order to detect any crack.

This inspection will make it possible to detect crack propagation at an early stage, thus avoiding an

expensive repair.

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.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 1

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 546011A01R03 2 3,360.00 Doubler, bolts

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 546011A01R03 2 3,360.00 Doubler, bolts

EFFECTIVITY

**CONF ALL

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

AAW ABD AMU F2I FDX JAL KAC KAL LAA MSR QTR SUD THA

UZB

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 54.51.41.001

OEB 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

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 2

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@A300-600

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 546011-832-801-001: Inspection

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 4.00

Task 546011-833-801-001: Repair

TOTAL MANHOURS 135.00

ELAPSED TIME (HOURS) 60.00

**CONF 002

Task 546011-832-801-001: Inspection

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 4.00

Task 546011-833-801-001: Repair

TOTAL MANHOURS 135.00

ELAPSED TIME (HOURS) 60.00

APPENDICES

**CONF ALL

APPENDIX 01

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 3

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@A300-600

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

A

LOWER SPAR AREAS TO BE INSPECTED

LOOKING OUTBOARD

RIB1 RIB5 RIB9 RIB10

FWD B

D_SB_546011_5_SAAA_01_00

B

A

Figure A-FSAAA - Sheet 01

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 4

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

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: 54

TITLE: NACELLES/PYLON - INSPECT PYLON LOWER SPAR BETWEEN RIBS

9 AND 10

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

B4-620 B4-622 B4-622R C4-620

(2) Effectivity by MSN

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365

0388 0417 0477 0479 0529-0530 0536 0543 0554-0555 0557 0559-0561 0566 0569

0572 0575 0577 0579 0581-0582 0601-0602 0607 0609 0611 0613-0614 0616-0617

0621 0625 0627-0631 0633 0635 0637 0641 0657 0659 0662 0664 0666 0668 0670

0677 0679 0681 0683 0685 0688 0692 0703 0705 0711 0717 0722 0724

(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.

OPERATOR MSN

AAW 0354

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 1

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@A300-600

SERVICE BULLETIN

OPERATOR MSN

ABD 0529 0557

AMU 0677

F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0637 0711

0724

FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559

0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664

0668 0688

JAL 0602 0617 0621 0641 0670 0679 0683 0703

KAC 0344

KAL 0582 0609 0627 0631 0662 0685 0692

LAA 0601 0616

MSR 0561 0607

QTR 0554 0560 0614

SUD 0666

THA 0566 0569 0577 0628 0629 0635 0681 0705

UZB 0717 0722

(4) Configuration by MSN

MSN CONFIGURATION

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351

0354

001

0358 0361 0365 0388 0417 0477 0479 0529 0530 0536 0543

0554 0555 0557 0559 0560 0561 0566 0569 0572 0575 0577

0579 0581 0582 0601 0602 0607 0609 0611 0613 0614 0616

0617 0621 0625 0627 0628 0629 0630 0631 0633 0635 0637

0641 0657 0659 0662 0664 0666 0668 0670 0677 0679 0681

0683 0685 0688 0692 0703 0705 0711 0717 0722 0724

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Mod. No. 04803S5726 (COCKPIT STYLING

AND COCKPIT WALL RELOCATION AND ASSOCIATED MODS) is not embodied.

**CONF 002

Config. 002 is valid for aircraft on which Mod. No. 04803S5726 is embodied.

NOTE: Config. 001 and 002 have been created because there is a difference in the

location of the circuit breakers to be opened/closed in this Service Bulletin.

The inspection and the repair described in this Service Bulletin are identical

for both configurations.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 546011A01R03 2

Consumable CMLA01 1

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 2

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SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

On aircraft fitted with Pratt and Whitney pylon, crack has been reported on pylon lower

spar.

The crack is running between ribs 9 and 10 and is starting on the center stiffener after

the flat area.

(2) Objective/Action

The aim of this Service Bulletin is to call for eddy current or liquid penetrant inspection of

the pylon lower spar in order to detect any crack.

(3) Advantages

This inspection will make it possible to detect crack propagation at an early stage, thus

avoiding an expensive repair.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 546011-832-801-001: Inspection

(1) Do a Special Detailed Inspection of the lower spar on engine 1 pylon

(2) Do a Special Detailed Inspection of the lower spar on engine 2 pylon

(3) Do a Special Detailed Inspection of the lower spar on engine 1 pylon (after

embodiment of the repair)

(4) Do a Special Detailed Inspection of the lower spar on engine 2 pylon (after

embodiment of the repair)

(5) Do a Special Detailed Inspection of the lower spar on engine 1 pylon (after

accomplishment of Service Bulletin No. A300-54-6019)

(6) Do a Special Detailed Inspection of the lower spar on engine 2 pylon (after

accomplishment of Service Bulletin No. A300-54-6019)

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 3

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SERVICE BULLETIN

Task 546011-833-801-001: Repair

(1) Do the Reinforcement of the lower spar on engine 1 pylon

(2) Do the Reinforcement of the lower spar on engine 2 pylon

**CONF 002

Task 546011-832-801-001: Inspection

(1) Do a Special Detailed Inspection of the lower spar on engine 1 pylon

(2) Do a Special Detailed Inspection of the lower spar on engine 2 pylon

(3) Do a Special Detailed Inspection of the lower spar on engine 1 pylon (after

embodiment of the repair)

(4) Do a Special Detailed Inspection of the lower spar on engine 2 pylon (after

embodiment of the repair)

(5) Do a Special Detailed Inspection of the lower spar on engine 1 pylon (after

accomplishment of Service Bulletin No. A300-54-6019)

(6) Do a Special Detailed Inspection of the lower spar on engine 2 pylon (after

accomplishment of Service Bulletin No. A300-54-6019)

Task 546011-833-801-001: Repair

(1) Do the Reinforcement of the lower spar on engine 1 pylon

(2) Do the Reinforcement of the lower spar on engine 2 pylon

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 4

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SERVICE BULLETIN

Compliance time (whichever occurs

later)

Configuration /

Condition

Action

Threshold Grace Period

Repetitive interval

(not to exceed)

Threshold 1 :

4,000 Flight Cycles

(FC)

- Interval 1 : 2,500

FC

CONF 001 and

002

Do a special

detailed inspection

in the lower spar

axis between Rib9

and Rib10 as

described in

SUBTASK

546011-832-001

001 and SUBTASK

546011-832-002

001

Threshold 2 :

4,000 FC

- Interval 2 : 2,500

FC

Crack is found Do the second

inspection as

described in

SUBTASK

546011-832-001

001 and SUBTASK

546011-832-002

001

Before next flight - -

Do the inspection

again as described

in SUBTASK

546011-832-001

001 and SUBTASK

546011-832-002

001

Interval not exceeding 2,500 FC -

OR

No crack is found

after the first or

second inspection

Apply Service

Bulletin No.

A300-54-6019

Before next flight - -

Crack is found with

dimensions

superior to 30mm

(1.181in.) after the

second inspection

Contact AIRBUS

and follow their

corrective action

Before next flight - -

Crack is found with

dimensions inferior

or equal to 30mm

(1.181in.) after the

second inspection

Do the

intermediate

inspection as

described in

SUBTASK

546011-832-001

001 and SUBTASK

546011-832-002

001

250 FC - -

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 5

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SERVICE BULLETIN

Compliance time (whichever occurs

later)

Configuration /

Condition

Action

Threshold Grace Period

Repetitive interval

(not to exceed)

Crack is found with

dimensions

superior or equal

to 30mm (1.181in.)

after the

intermediate

inspection.

Contact AIRBUS

and follow their

corrective action

Before next flight - -

Crack is found with

dimensions inferior

to 30mm (1.181in.)

after the

intermediate

inspection

Do the repair as

described in TASK

546011-833-801-001

250 FC - -

- Threshold 1 and Interval 1 concerns aircraft with an Average Flight Time (AFT) superior to 1.5

hours.

- Threshold 2 and Interval 2 concerns aircraft with an AFT inferior to 1.5 hours.

Accomplishment Timescale Table

Compliance time (whichever occurs

later)

Configuration /

Condition

Action

Threshold Grace Period

Repetitive interval

(not to exceed)

Grace Period 1 :

1,000 FC

Threshold 1 :

6,400 FC / 13,600

Flight Hours (FH) Grace Period 2 :

500 FC

Interval 1 : 4,300

FC

Grace Period 1 :

1,000 FC

CONF 001 and

002

Do a special

detailed inspection

in the lower spar

axis between Rib9

and Rib10 as

described in

SUBTASK

546011-832-003

001 and SUBTASK

546011-832-004

001

Threshold 2 :

7,100 FC / 10,600

FH Grace Period 2 :

500 FC

Interval 2 : 4,300

FC

Crack is found Contact AIRBUS

and follow their

corrective action

Before next flight - -

No crack is found Do the inspection

again as described

in SUBTASK

546011-832-003

001 and SUBTASK

546011-832-004

001

Interval not exceeding 4,300 FC -

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 6

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SERVICE BULLETIN

- Threshold counted from repair embodiment.

- Threshold 1 and Interval 1 concerns aircraft with an AFT superior to 1.5 hours.

- Threshold 2 and Interval 2 concerns aircraft with an AFT inferior to 1.5 hours.

- Grace period 1 is valid for aircraft that have already exceeded the values given in the table and

which have accumulated less than 21,400 FC (less than 23,900 FC for AFT inferior to 1.5 hours)

from the repair embodiment.

- Grace period 2 is valid for aircraft that have already exceeded the values given in the table and

which have accumulated more than 21,400 FC (more than 23,900 FC for AFT inferior to 1.5 hours)

from the repair embodiment.

Accomplishment Timescale Table for Aircraft with Repair Embodied

Compliance time (whichever occurs

later)

Configuration /

Condition

Action

Threshold Grace Period

Repetitive interval

(not to exceed)

Grace Period 1 :

2,000 FC

Threshold 1 :

7,400 FC / 15,700

Flight Hours (FH) Grace Period 2 :

1,000 FC

Interval 1 : 11,000

FC / 23,400 FH

Grace Period 1 :

2,000 FC

CONF 001 and

002

Do a special

detailed inspection

in the lower spar

axis between Rib9

and Rib10 as

described in

SUBTASK

546011-832-005

001 and SUBTASK

546011-832-006

001

Threshold 2 :

8,200 FC / 12,300

FH Grace Period 2 :

1,000 FC

Interval 2 : 12,200

FC / 18,300 FH

Crack is found Contact AIRBUS

and follow their

corrective action

Before next flight - -

Interval 1 not exceeding 11,000 FC /

23,400 FH

No crack is found Do the inspection

again as described

in SUBTASK

546011-832-005

001 and SUBTASK

546011-832-006

001

Interval 2 not exceeding 12,200 FC /

18,300 FH

-

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 7

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@A300-600

SERVICE BULLETIN

- Threshold counted from Service Bulletin No. A300-54-6019 embodiment.

- Threshold 1 and Interval 1 concerns aircraft with an AFT superior to 1.5 hours.

- Threshold 2 and Interval 2 concerns aircraft with an AFT inferior to 1.5 hours.

- Grace period 1 is valid for aircraft that have already exceeded the values given in the table and

which have accumulated less than 21,800 FC (less than 24,400 FC for AFT inferior to 1.5 hours)

from SB A300-54-6019 embodiment.

- Grace period 2 is valid for aircraft that have already exceeded the values given in the table and

which have accumulated more than 21,800 FC (more than 24,400 FC for AFT inferior to 1.5 hours)

from SB A300-54-6019 embodiment.

Accomplishment Timescale Table for Aircraft with Service Bulletin No. A300-54-6019 Accomplished

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.

**CONF 001

Task 546011-832-801-001: Inspection

Get Access 3.00

On Aircraft

Do a Special Detailed Inspection of the lower spar on

engine 1 pylon

1.00

Do a Special Detailed Inspection of the lower spar on

engine 2 pylon

1.00

Do a Special Detailed Inspection of the lower spar on

engine 1 pylon (after embodiment of the repair)

1.00

Do a Special Detailed Inspection of the lower spar on

engine 2 pylon (after embodiment of the repair)

1.00

Do a Special Detailed Inspection of the lower spar on

engine 1 pylon (after accomplishment of Service

Bulletin No. A300-54-6019)

1.00

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 8

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@A300-600

SERVICE BULLETIN

Task 546011-832-801-001: Inspection

Do a Special Detailed Inspection of the lower spar on

engine 2 pylon (after accomplishment of Service

Bulletin No. A300-54-6019)

1.00

Close-Up 3.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 4.00

NOTE: The TOTAL MANHOURS for each inspection is 8.00 hours.

Task 546011-833-801-001: Repair

Get Access 46.00

On Aircraft

Do the Reinforcement of the lower spar on engine 1

pylon

20.00

Do the Reinforcement of the lower spar on engine 2

pylon

20.00

Tests 3.00

Close-Up 46.00

TOTAL MANHOURS 135.00

ELAPSED TIME (HOURS) 60.00

**CONF 002

Task 546011-832-801-001: Inspection

Get Access 3.00

On Aircraft

Do a Special Detailed Inspection of the lower spar on

engine 1 pylon

1.00

Do a Special Detailed Inspection of the lower spar on

engine 2 pylon

1.00

Do a Special Detailed Inspection of the lower spar on

engine 1 pylon (after embodiment of the repair)

1.00

Do a Special Detailed Inspection of the lower spar on

engine 2 pylon (after embodiment of the repair)

1.00

Do a Special Detailed Inspection of the lower spar on

engine 1 pylon (after accomplishment of Service

Bulletin No. A300-54-6019)

1.00

Do a Special Detailed Inspection of the lower spar on

engine 2 pylon (after accomplishment of Service

Bulletin No. A300-54-6019)

1.00

Close-Up 3.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 4.00

NOTE: The TOTAL MANHOURS for each inspection is 8.00 hours.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 9

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@A300-600

SERVICE BULLETIN

Task 546011-833-801-001: Repair

Get Access 46.00

On Aircraft

Do the Reinforcement of the lower spar on engine 1

pylon

20.00

Do the Reinforcement of the lower spar on engine 2

pylon

20.00

Tests 3.00

Close-Up 46.00

TOTAL MANHOURS 135.00

ELAPSED TIME (HOURS) 60.00

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-54 24-00-00 24-41-00

24-50-20 71-00-00

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

Non Destructive Test Manual (NTM) 54-50-40

Service Bulletin (SB) A300-54-6019

Standards Manual (SM)

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-54 24-00-00 24-41-00

24-50-20 71-00-00

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

Non Destructive Test Manual (NTM) 54-50-40

Service Bulletin (SB) A300-54-6019

Standards Manual (SM)

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 10

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SERVICE BULLETIN

M. SPARES

None

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 11

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 12

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@A300-600

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 546011A01R03 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 by E-mail :

airbus.kit@airbus.com

(2) Price and Availability

Kit 546011A01R03

Cost 1,680.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

Kit 546011A01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

NAS1726C3E NUT

NAS6703U5 BOLT

NAS6703U6 BOLT

NAS6703U6X BOLT

NSA5415-40-10 RIVET

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 13

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

R5460002920200 FILLER

R5460003020400 DOUBLER

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Service Bulletin it is necessary to use the tools listed in NTM

54-50-40 Part 6 and NTM 54-50-40 Part 9.

(3) Special Tools

None

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 14

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 546011-832-801-001 - 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

Zone

410 420

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 4.00

**CONF 002

Zone

410 420

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 4.00

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 15

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SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 546011-839-001-001 - 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 546011-839-001-001 - 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 546011-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

24-50-20, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put the access platform(s) in position.

(d) Open the pylon lateral access doors 415AL, 416AR, 425AL and 426AR (Refer to

AMM 06-41-54, Page Block 001).

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 16

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@A300-600

SERVICE BULLETIN

(e) Open, safety/lock and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

123VU ENG1 & 2/IGNITION/SYS B 2JH (01)

123VU ENG1 & 2/IGNITION/SYS A 1JH (01)

123VU ENG1 & 2/START/CTL/WARN 1KG (01)

NOTE (01): For the location of the circuit breakers refer to AMM 24-50-20, Page

Block 001.

**CONF 002

(1) Subtask 546011-941-001-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

24-50-20, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put the access platform(s) in position.

(d) Open the pylon lateral access doors 415AL, 416AR, 425AL and 426AR (Refer to

AMM 06-41-54, Page Block 001).

(e) Open, safety/lock and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU ENG1 & 2/IGNITION/SYS B 2JH (01)

133VU ENG1 & 2/IGNITION/SYS A 1JH (01)

133VU ENG1 & 2/START/CTL/WARN 1KG (01)

133VU ENGINES/ENG2/IGNITION/

SYS A

8JH (01)

NOTE (01): For the location of the circuit breakers refer to AMM 24-50-20, Page

Block 001.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 17

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 546011-832-001-001 - Do a Special Detailed Inspection of the lower spar

on engine 1 pylon

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBAAA

Area to be Inspected

Sheet 01

(a) For the inspection area, refer to Fig. A-FBAAA Sheet 01.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 1 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(2) Subtask 546011-832-002-001 - Do a Special Detailed Inspection of the lower spar

on engine 2 pylon

Work Zones and Access Panels

Zone Access/Work location

420

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 18

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

(a) For the inspection area, refer to Fig. A-FBAAA Sheet 01.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 2 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(3) Subtask 546011-832-003-001 - Do a Special Detailed Inspection of the lower spar

on engine 1 pylon (after embodiment of the repair)

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FBBAA

Area to be Inspected (after embodiment

of the repair)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft repaired as per

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 19

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@A300-600

SERVICE BULLETIN

instructions given in this Service Bulletin.

(a) For the inspection area, refer to Fig. A-FBBAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 1 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(4) Subtask 546011-832-004-001 - Do a Special Detailed Inspection of the lower spar

on engine 2 pylon (after embodiment of the repair)

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FBBAA

Area to be Inspected (after embodiment

of the repair)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft repaired as per

instructions given in this Service Bulletin.

(a) For the inspection area, refer to Fig. A-FBBAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 2 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 20

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SERVICE BULLETIN

(5) Subtask 546011-832-005-001 - Do a Special Detailed Inspection of the lower spar

on engine 1 pylon (after accomplishment of Service Bulletin No. A300-54-6019)

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Service Bulletin (SB) A300-54-6019

Fig. A-FBCAA

Area to be Inspected (after

accomplishment of Service Bulletin No.

A300-54-6019)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft on which Service

Bulletin No. A300-54-6019 is embodied.

(a) For the inspection area, refer to Fig. A-FBCAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 1 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(6) Subtask 546011-832-006-001 - Do a Special Detailed Inspection of the lower spar

on engine 2 pylon (after accomplishment of Service Bulletin No. A300-54-6019)

Work Zones and Access Panels

Zone Access/Work location

420

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 21

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Service Bulletin (SB) A300-54-6019

Fig. A-FBCAA

Area to be Inspected (after

accomplishment of Service Bulletin No.

A300-54-6019)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft on which Service

Bulletin No. A300-54-6019 is embodied.

(a) For the inspection area, refer to Fig. A-FBCAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 2 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

**CONF 002

(1) Subtask 546011-832-001-001 - Do a Special Detailed Inspection of the lower spar

on engine 1 pylon

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 22

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@A300-600

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References

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBAAA

Area to be Inspected

Sheet 01

(a) For the inspection area, refer to Fig. A-FBAAA Sheet 01.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 1 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(2) Subtask 546011-832-002-001 - Do a Special Detailed Inspection of the lower spar

on engine 2 pylon

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

(a) For the inspection area, refer to Fig. A-FBAAA Sheet 01.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 2 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 23

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@A300-600

SERVICE BULLETIN

(3) Subtask 546011-832-003-001 - Do a Special Detailed Inspection of the lower spar

on engine 1 pylon (after embodiment of the repair)

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FBBAA

Area to be Inspected (after embodiment

of the repair)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft repaired as per

instructions given in this Service Bulletin.

(a) For the inspection area, refer to Fig. A-FBBAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 1 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(4) Subtask 546011-832-004-001 - Do a Special Detailed Inspection of the lower spar

on engine 2 pylon (after embodiment of the repair)

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 24

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@A300-600

SERVICE BULLETIN

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Fig. A-FBBAA

Area to be Inspected (after embodiment

of the repair)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft repaired as per

instructions given in this Service Bulletin.

(a) For the inspection area, refer to Fig. A-FBBAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 2 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(5) Subtask 546011-832-005-001 - Do a Special Detailed Inspection of the lower spar

on engine 1 pylon (after accomplishment of Service Bulletin No. A300-54-6019)

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Service Bulletin (SB) A300-54-6019

Fig. A-FBCAA

Area to be Inspected (after

accomplishment of Service Bulletin No.

A300-54-6019)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft on which Service

Bulletin No. A300-54-6019 is embodied.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 25

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SERVICE BULLETIN

(a) For the inspection area, refer to Fig. A-FBCAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 1 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

(6) Subtask 546011-832-006-001 - Do a Special Detailed Inspection of the lower spar

on engine 2 pylon (after accomplishment of Service Bulletin No. A300-54-6019)

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40 Part 6

54-50-40 Part 9

Service Bulletin (SB) A300-54-6019

Fig. A-FBCAA

Area to be Inspected (after

accomplishment of Service Bulletin No.

A300-54-6019)

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

NOTE: This inspection has to be performed only on aircraft on which Service

Bulletin No. A300-54-6019 is embodied.

(a) For the inspection area, refer to Fig. A-FBCAA.

(b) Do a special detailed inspection of the lower spar between ribs 09 and 10 on

engine 2 pylon as per NTM 54-50-40 Part 6 (High Frequency Eddy Current

(HFEC)) or NTM 54-50-40 Part 9 (Liquid penetrant inspection), refer to Fig. AFFAAA Sheet 01, Fig. A-FFAAA Sheet 02 and Fig. A-FFAAA Sheet 03.

(c) For the inspection report, refer to APPENDIX 01 .

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 26

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 546011-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-50-20, Page Block 001

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

equipment.

(b) Close the pylon lateral access doors 415AL, 416AR, 425AL and426AR (Refer to

AMM 06-41-54, Page Block 001).

(c) Remove the safety clips and/or tags and close/unlock these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

123VU ENG1 & 2/IGNITION/SYS B 2JH (01)

123VU ENG1 & 2/IGNITION/SYS A 1JH (01)

123VU ENG1 & 2/START/CTL/WARN 1KG (01)

NOTE (01): For the location of the circuit breakers refer to AMM 24-50-20, Page

Block 001.

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 27

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**CONF 002

(1) Subtask 546011-942-001-002 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-50-20, Page Block 001

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

equipment.

(b) Close the pylon lateral access doors 415AL, 416AR, 425AL and426AR (Refer to

AMM 06-41-54, Page Block 001).

(c) Remove the safety clips and/or tags and close/unlock these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU ENG1 & 2/IGNITION/SYS B 2JH (01)

133VU ENG1 & 2/IGNITION/SYS A 1JH (01)

133VU ENG1 & 2/START/CTL/WARN 1KG (01)

133VU ENGINES/ENG2/IGNITION/

SYS A

8JH (01)

NOTE (01): For the location of the circuit breakers refer to AMM 24-50-20, Page

Block 001.

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 28

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SERVICE BULLETIN

Task 546011-833-801-001 - Repair

**CONF ALL

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

Zone

410 420

Manpower

TOTAL MANHOURS 135.00

ELAPSED TIME (HOURS) 60.00

**CONF 002

Zone

410 420

Manpower

TOTAL MANHOURS 135.00

ELAPSED TIME (HOURS) 60.00

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 29

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SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 546011-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

(a) Clean the surfaces to be sealed with :

Solvent General

Purpose

11-026 As required

(2) Subtask 546011-839-002-001 - 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 546011-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

(a) Clean the surfaces to be sealed with :

Solvent General

Purpose

11-026 As required

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 30

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SERVICE BULLETIN

(2) Subtask 546011-839-002-001 - 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 546011-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301

71-00-00, Page Block 401

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position.

(c) Remove the LH and RH power plant (Refer to AMM 71-00-00, Page Block 401).

**CONF 002

(1) Subtask 546011-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301

71-00-00, Page Block 401

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position.

(c) Remove the LH and RH power plant (Refer to AMM 71-00-00, Page Block 401).

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 31

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 546011-833-001-001 - Do the Reinforcement of the lower spar on engine 1

pylon

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 20.00

Minimum number of person 1

Subtask elapsed time 20.00

Skills AIRFRAME

(a) Do the reinforcement of the lower spar as described in Drawing 41R54600029,

Sheet 1, issue I and Sheet 2, issue D.

Use Kit 546011A01R03

NOTE: Kit Kit 546011A01R03 is valid for one pylon.

(2) Subtask 546011-833-002-001 - Do the Reinforcement of the lower spar on engine 2

pylon

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 20.00

Minimum number of person 1

Subtask elapsed time 20.00

Skills AIRFRAME

(a) Do the reinforcement of the lower spar as described in Drawing 41R54600029,

Sheet 1, issue I and Sheet 2, issue D.

Use Kit 546011A01R03

NOTE: Kit Kit 546011A01R03 is valid for one pylon.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 32

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SERVICE BULLETIN

**CONF 002

(1) Subtask 546011-833-001-001 - Do the Reinforcement of the lower spar on engine 1

pylon

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 20.00

Minimum number of person 1

Subtask elapsed time 20.00

Skills AIRFRAME

(a) Do the reinforcement of the lower spar as described in Drawing 41R54600029,

Sheet 1, issue I and Sheet 2, issue D.

Use Kit 546011A01R03

NOTE: Kit Kit 546011A01R03 is valid for one pylon.

(2) Subtask 546011-833-002-001 - Do the Reinforcement of the lower spar on engine 2

pylon

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 20.00

Minimum number of person 1

Subtask elapsed time 20.00

Skills AIRFRAME

(a) Do the reinforcement of the lower spar as described in Drawing 41R54600029,

Sheet 1, issue I and Sheet 2, issue D.

Use Kit 546011A01R03

NOTE: Kit Kit 546011A01R03 is valid for one pylon.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 33

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 546011-700-002-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 71-00-00, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the LH and RH power plant (Refer to AMM 71-00-00,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the LH and RH

power plant (Refer to AMM 71-00-00, Page Block 401).

**CONF 002

(1) Subtask 546011-700-002-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 71-00-00, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the LH and RH power plant (Refer to AMM 71-00-00,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the LH and RH

power plant (Refer to AMM 71-00-00, Page Block 401).

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 34

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 546011-942-002-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

410

420

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 71-00-00, Page Block 401

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

equipment.

(b) Install the LH and RH power plant (Refer to AMM 71-00-00, Page Block 401).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

**CONF 002

(1) Subtask 546011-942-002-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

410

420

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 71-00-00, Page Block 401

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

equipment.

(b) Install the LH and RH power plant (Refer to AMM 71-00-00, Page Block 401).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 35

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SERVICE BULLETIN

**CONF ALL

AREAS TO BE INSPECTED

LOWER SPAR

D_SB_546011_5_BAAA_01_00

A

A

RIB18

RIB12

RIB10

RIB9

RIB8

B

A

RIB8 RIB9 RIB10

FWD

B

NOTE:

Figure A-FBAAA - Sheet 01

Area to be Inspected

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 36

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SERVICE BULLETIN

**CONF ALL

LOWER SPAR

A

A

RIB18

RIB12

RIB10

RIB9

RIB8

B

A

RIB8 RIB9 RIB10

FWD

B

D_SB_546011_5_BBAA_01_00

AREAS TO BE INSPECTED

NOTE:

Figure A-FBBAA - Sheet 01

Area to be Inspected (after embodiment of the repair)

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 37

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SERVICE BULLETIN

**CONF ALL

LOWER SPAR

A

A

RIB18

RIB12

RIB10

RIB9

RIB8

B

A

RIB8 RIB9 RIB10

FWD

B

D_SB_546011_5_BCAA_01_00

AREAS TO BE INSPECTED

NOTE:

Figure A-FBCAA - Sheet 01

Area to be Inspected (after accomplishment of Service Bulletin No. A300-54-6019)

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 38

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SERVICE BULLETIN

**CONF ALL

QUESTION

FINDING

ACTION

CRACK FOUND NO

DO A SPECIAL DETAILED INSPECTION (HFEC INSPECTION AS PER NTM 54−50−40

PART 6 OR LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40 PART 9)

IN THE LOWER SPAR AXIS BETWEEN RIB9 AND RIB10 FROM THE INSIDE,

AT THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2).

(REFER TO FIGURE A−FBAAA)

YES

(HFEC INSPECTION AS PER NTM 54−50−40 PART 6 AND

LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40

PLANNING INFORMATION PARAGRAPH E.(2).

(REFER TO FIGURE A−FBAAA)

DO THE SPECIAL DETAILED INSPECTION AGAIN

PART 9) AT THRESHOLD GIVEN IN

ALUMINIUM SPRAY PROTECTION (0.17 mm (0.007 in.)

THEORETICAL THICKNESS)

SMOOTH BLEND OUT THE AREA TO REMOVE THE

AREA BY PAD CADMIUM PLATING

(REFER TO SRM 51−21−10)

RENEW THE PROTECTION OF THE

YES CRACK FOUND NO

REFER TO FIGURE

A−FFAAA SHEET 03

REFER TO FIGURE

A−FFAAA SHEET 02

D_SB_546011_5_FAAA_01_02

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 39

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SERVICE BULLETIN

**CONF ALL

QUESTION ACTION FINDING

YES CRACK 30 mm (1.181 in) NO

OR LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40 PART 9

(REFER TO FIGURE A−FBAAA)

AT THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

DO THE REPAIR AS DESCRIBED IN TASK 546011−833−801−001

CRACK 30 mm (1.181 in)

NO

YES

DO AN INTERMEDIATE HFEC INSPECTION AS PER NTM 54−50−40 PART 6

FROM FIGURE

A−FFAAA SHEET 01

LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40 PART 9

(REFER TO FIGURE A−FBBAA)

AT THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

DO AN HFEC INSPECTION AS PER NTM 54−50−40 PART 6 OR A

CRACK FOUND

NO

LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40 PART 9

(REFER TO FIGURE A−FBBAA)

AT INTERVAL GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

DO AN HFEC INSPECTION AS PER NTM 54−50−40 PART 6 OR A

YES

CONTACT AIRBUS

AND FOLLOW THEIR

CORRECTIVE ACTION

D_SB_546011_5_FAAA_02_00

Figure A-FFAAA - Sheet 02

Flow Chart

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 40

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SERVICE BULLETIN

**CONF ALL

QUESTION ACTION FINDING

(MOD. No. 10328S20412)

FROM FIGURE

A−FFAAA SHEET 01

LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40 PART 9

(REFER TO FIGURE A−FBCAA)

AT THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

DO AN HFEC INSPECTION AS PER NTM 54−50−40 PART 6 OR A

CRACK FOUND

NO

LIQUID PENETRANT INSPECTION AS PER NTM 54−50−40 PART 9

(REFER TO FIGURE A−FBCAA)

AT INTERVAL GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

DO AN HFEC INSPECTION AS PER NTM 54−50−40 PART 6 OR A

D_SB_546011_5_FAAA_03_00

YES

CONTACT AIRBUS

AND FOLLOW THEIR

CORRECTIVE ACTION

No. A300−54−6019

OR

APPLY SERVICE BULLETIN

INFORMATION PARAGRAPH E.(2)

INTERVAL GIVEN IN PLANNING

DO THE INSPECTION AGAIN AT

Figure A-FFAAA - Sheet 03

Flow Chart

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 41

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 42

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SERVICE BULLETIN

APPENDIX 01

**CONF ALL

(1) The result of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS Department SEES2, on the attached inspection report sheet.

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 1

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SERVICE BULLETIN

APPENDIX 01

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−54−6011

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRUCTURE − ENGINE PYLON

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX : +33 (0)5 61 93 36 14

NO CRACK

PYLON LEFT

AREA 1

AREA 2

PYLON RIGHT

AREA 1

AREA 2

LENGTH DEPTH

CRACK

LENGTH

DEPTH

CENTER

STIFFENER

AREA 1 OR 2

D_SB_546011_5_RAAA_01_00

A

A

AREA 1 AREA 2

RIB9 RIB10

FWD

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 2

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SERVICE BULLETIN

APPENDIX 01

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−54−6011

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD :

NO CRACK

PYLON LEFT

AREA 1

AREA 2

PYLON RIGHT

AREA 1

AREA 2

LENGTH DEPTH

CRACK

CENTER

STIFFENER

RIB9 RIB10

FWD

D_SB_546011_5_RAAA_02_00

AREA 2 AREA 1

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRUCTURE − ENGINE PYLON

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX : +33 (0)5 61 93 36 14

Figure A-FRAAA - Sheet 02

Inspection Report

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 3

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SERVICE BULLETIN

APPENDIX 01

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−54−6011

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD :

NO CRACK

PYLON LEFT

AREA 1

AREA 2

PYLON RIGHT

AREA 1

AREA 2

LENGTH DEPTH

CRACK

CENTER

STIFFENER

RIB9 RIB10

FWD

AREA 2

D_SB_546011_5_RAAA_03_00

AREA 1 FASTENERS

TO BE INSPECTED

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRUCTURE − ENGINE PYLON

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX : +33 (0)5 61 93 36 14

Figure A-FRAAA - Sheet 03

Inspection Report

DATE: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 4

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SERVICE BULLETIN

REPORTING SHEET

TITLE: NACELLES/PYLON - INSPECT PYLON LOWER SPAR BETWEEN RIBS

9 AND 10

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: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

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: Nov 12/91 SERVICE BULLETIN No.: A300-54-6011

REVISION No.: 03 - Jun 23/11 Page: 1

5

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