@A310

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.06 of Service Bulletin No.A310-54-2016

ADDITIONAL WORK

**CONF ALL

NOTE: No additional work is required by this revision for aircraft modified by any previous

issue.

REASON

Revision No. 06 issued to remove aircraft with GE engine and aircraft with MOD 10149S20315

embodied.

CHANGES

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

CONF 002 CONFIGURATION DEFINITION UPDATED R

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.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to inform the operators of the addition of technical information.

Revision No. 02 issued to reduce the inspection thresholds and intervals of Inspection Service Bulletin

No. A310-54-2016, add inspection after accomplishment of Service Bulletin No. A310-54-2022 (Mod.

No. 10328S20412).

Revision No. 03 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).

Revision No. 04 issued to reduce the inspection thresholds and intervals.

Revision No. 05 issued to modify the thresholds and intervals following analysis improvement and inserving crack findings consistency.

REVISION SEQUENCE

ORIGINAL: Nov 12/91

REVISION No.: 01 - Oct 15/93

REVISION No.: 02 - Jun 11/99

REVISION No.: 03 - Aug 25/00

REVISION No.: 04 - Nov 16/07

REVISION No. : 05 - Oct 05/12

REVISION No. : 06 - Jan 16/13

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 2

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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 & WHITHNEY 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.

This Inspection Service Bulletin was first modified in the frame of the A310 Aircraft Extended Service

Goal study, but some cracks have been reported re-initiating even after Service Bulletin embodiment.

Hence a deeper investigation has been performed on order to propose the best alternative solution to

the operators.

This Inspection Service Bulletin requires an Eddy current or a 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 a

significant repair and reduction of the structural capacity.

New Flight Cycles / Flight Hours figures of Threshold and Intervals, due to improvement of analyses

and also consistent with in-service crack findings, were acknowledge by Airworthiness Authorities.

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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 1

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

ENGINE REMOVAL YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 542016A01R02 2 2,560.00 Doubler, Filler

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 542016A01R02 2 2,560.00 Doubler, Filler

EFFECTIVITY

**CONF ALL

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

19U 52X 85W 99Y AIB AIC BAF BBC FDX IYE JAV PCA PIA

R1T ROT RZO SUD UBD UZB

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 54.51.41.001

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 542016-832-801-001: Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 542016-832-803-001: Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 542016-833-802-001: Repair

TOTAL MANHOURS 52.00

ELAPSED TIME (HOURS) 28.00

**CONF 002

Task 542016-832-801-001: Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 542016-832-803-001: Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 542016-833-802-001: Repair

TOTAL MANHOURS 52.00

ELAPSED TIME (HOURS) 28.00

APPENDICES

**CONF ALL

Appendix 01: Inspection Report

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

SUMMARY

**CONF ALL

A

B

A

A

B

LOOKING OUTBOARD

RIB 1 RIB 5 RIB 9 RIB 10

LOWER SPAR

AREAS TO BE INSPECTED

B_SB_542016_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 4

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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: 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

NOTE: This Inspection Service Bulletin is applicable only to A310 aircraft equipped

with PRATT & WHITNEY JT9D-7R4 and PRATT & WHITNEY 4000 engines.

NOTE (01): This Inspection Service Bulletin is only applicable to A310 aircraft on

which modification No. 10149S20315 (NACELLES/PYLONS - ENGINE

PYLON PRIMARY STRUCTURE MODIFY LOWER SPAR) is not embodied

(production scheme).

Modification No. 10149S20315 (production scheme) is embodied before

delivery on A310 aircraft MSN 0691 and subsequent.

(1) Models

310-221 310-222 310-322 310-324 310-325

(2) Effectivity by MSN

0162 0217 0224 0251 0260 0267 0278 0288 0303 0313 0318 0331 0333 0339

0342-0343 0345-0346 0357 0367 0372 0378 0399 0410 0419 0437 0439 0449 0452

0456-0458 0467 0489 0492 0500 0534 0539 0542 0549 0568 0574 0576 0591 0594

0624 0636 0638 0642 0644 0654 0660 0669 0672 0674 0676 0678 0682 0684

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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@A310

SERVICE BULLETIN

0686-0687 0689

(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

19U 0399

52X 0410

85W 0684

99Y 0489

AIB 0686

AIC 0654 0669

BAF 0367 0372

BBC 0594 0642

FDX 0162 0217 0224 0251 0260 0267 0278 0288 0303 0313 0318 0331

0333 0339 0342 0343 0345 0346 0378 0439 0449 0452 0456 0457

0458 0467 0492 0500 0534 0539 0542 0549 0638

IYE 0568

JAV 0357

PCA 0419

PIA 0660 0676 0678 0682 0687 0689

R1T 0591

ROT 0636 0644

RZO 0624

SUD 0437

UBD 0672 0674

UZB 0574 0576

(4) Configuration by MSN

MSN CONFIGURATION

0162 0217 0224 0251 0260 0267 0278 0288 0303 0313 0318

0331 0333 0339 0342 0343 0345 0346 0357 0367 0372 0419

001

0378 0399 0410 0437 0439 0449 0452 0456 0457 0458 0467

0489 0492 0500 0534 0539 0542 0549 0568 0574 0576 0591

0594 0624 0636 0638 0642 0644 0654 0660 0669 0672 0674

0676 0678 0682 0684 0686 0687 0689

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for the aircraft model A310-221 and A310-222.

**CONF 002

Config. 002 is valid for the aircraft model A310-322, A310-324 and A310-325.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 542016A01R02 2

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

On aircraft fitted with PRATT & WHITHNEY 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.

This Inspection Service Bulletin was first modified in the frame of the A310 Aircraft

Extended Service Goal study, but some cracks have been reported re-initiating even

after Service Bulletin embodiment. Hence a deeper investigation has been performed on

order to propose the best alternative solution to the operators.

(2) Objective/Action

This Inspection Service Bulletin requires an Eddy current or a 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 a significant repair and reduction of the structural capacity.

New Flight Cycles / Flight Hours figures of Threshold and Intervals, due to improvement

of analyses and also consistent with in-service crack findings, were acknowledge by

Airworthiness Authorities.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 542016-832-801-001: Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

(1) Do a Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair and Pre SB

54-2022.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

(2) Do a Special Detailed Inspection of the LH/RH Engine Pylon without protection.

(3) Do an Intermediate Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair

and Pre-SB 54-2022.

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

(1) Do a Special Detailed Inspection of the LH/RH Engine Pylon Post-repair.

Task 542016-832-803-001: Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

(1) Do a Special Detailed Inspection of the LH/RH Engine Pylon Post SB 54-2022.

Task 542016-833-802-001: Repair

(1) Reinforce the Lower Spar with a Doubler.

**CONF 002

Task 542016-832-801-001: Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

(1) Do a Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair and Pre SB

54-2022.

(2) Do a Special Detailed Inspection of the LH/RH Engine Pylon without protection.

(3) Do an Intermediate Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair

and Pre-SB 54-2022.

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

(1) Do a Special Detailed Inspection of the LH/RH Engine Pylon Post-repair.

Task 542016-832-803-001: Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

(1) Do a Special Detailed Inspection of the LH/RH Engine Pylon Post SB 54-2022.

Task 542016-833-802-001: Repair

(1) Reinforce the Lower Spar with a Doubler.

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

(2) Accomplishment Timescale

**CONF 001

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.

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace Period

Repetitive

Interval (FC or

FH whichever

occurs first)

Conf. 001 Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Pre-repair

and Pre-SB 54-2022 Refer

to Subtask

542016-832-012-001.

3,300 FC /6,600

FH

None None

Do Re-Inspection of the

LH/RH Engine Pylon Prerepair and Pre-SB 54-2022

Refer to Subtask

542016-832-012-001.

None None 2,300 FC /

4,700 FH

Or

Apply the SB 54-2022. Before next flight None None

And

No crack found

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to Subtask

542016-832-016-001.

Refer to table 2

Crack found Do a Special Detailed

Inspection of the LH/RH

Engine Pylon without the

aluminium spray protection

Refer to Subtask

542016-832-014-001.

Before next flight None None

Do Re-Inspection of the

LH/RH Engine Pylon Prerepair and Pre-SB 54-2022

Refer to Subtask

542016-832-012-001.

None None 2,300 FC /

4,700 FH

Or

Apply the SB 54-2022. Before next flight None None

And

No crack found after

embodiment of

Subtask

542016-832-014-001.

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to Subtask

542016-832-016-001.

Refer to table 2

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace Period

Repetitive

Interval (FC or

FH whichever

occurs first)

Crack found < or = 30

mm (1.181 in.) after

embodiment of

Subtask

542016-832-014-001.

Do an Intermediate

Special Detailed

Inspection of the LH/RH

Engine Pylon Pre-repair

and Pre-SB 54-2022 Refer

to Subtask

542016-832-015-001.

250 FC None None

Crack found > 30 mm

(1.181 in.) after

embodiment of

Subtask

542016-832-014-001.

Contact AIRBUS Before next flight None None

Install the doubler on the

LH and/or RH Pylon Refer

to Subtask

542016-833-020-001.

Before 250 FC None None

And

Crack found < or = 30

mm (1.181 in.) after

embodiment of

Subtask

542016-832-015-001.

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post repair

Refer to Subtask

542016-832-017-001.

Refer to table 3

Crack found > 30 mm

(1.181 in.) after

embodiment of

Subtask

542016-832-015-001.

Contact AIRBUS Before next flight None None

Table 1, Special Detailed Inspection between RIB9 and RIB10 Pre-repair and Pre-SB 54-2022 for

A310-200 aircraft.

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

Conf . 001

After

accomplishment

of SB 54-2022

(10328S20412).

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to

Subtask

542016-832-016-001.

5,100 FC / 10,200

FH

see notes (01)

and (02)

None

Crack found. Contact AIRBUS Before next flight None None

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

No crack found Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to

Subtask

542016-832-016-001.

None see notes (01)

and (02)

9,200 FC /

18,400 FH

Table 2, Special Detailed Inspection between RIB9 and RIB10 for A310-200 aircraft Post SB 54-2022.

NOTE (01): For A310-200 aircraft with Service Bulletin No. A310-54-2022

accomplished less than 16,800 FC from Service Bulletin No.

A310-54-2022 accomplishment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 2,000 FC

is applicable from publication date as long as this value does not

exceed the previous figures.

NOTE (02): For A310-200 aircraft with Service Bulletin No. A310-54-2022

accomplished more than 16,800 FC from Service Bulletin No.

A310-54-2022 accomplishment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 1,000 FC

is applicable from publication date as long as this value does not

exceed the previous figures.

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

Conf . 001

After the

Installation of

the doubler on

the LH and/or

RH Pylon.

Do a Special Inspection

of the LH/RH Engine

Pylon Post repair Refer

to Subtask

542016-832-017-001.

4,400 FC / 8,800

FH

see notes (03) and

(04)

None

Crack found Contact AIRBUS Before next flight None None

No crack found Do a Special Inspection

of the LH/RH Engine

Pylon Post repair Refer

to Subtask

542016-832-017-001.

None see notes (03) and

(04)

2,800 FC / 5,700

FH

Table 3, Special Detailed Inspection between RIB9 and RIB10 for A310-200 aircraft Post repair .

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SERVICE BULLETIN

NOTE (03): For A310-200 aircraft less than 16,700 FC from repair embodiment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 1,000 FC

is applicable for repaired A310-200 aircraft from publication date as

long as this value does not exceed the previous figures.

NOTE (04): For A310-200 aircraft more than 16,700 FC from repair embodiment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 500 FC

is applicable for repaired A310-200 aircraft from publication date as

long as this value does not exceed the previous figures.

**CONF 002

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.

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

SR:

2,700 FC /7,600

FH

Config. 002 Do a Special Detailed None

Inspection of the LH/RH

Engine Pylon Pre-repair

and Pre-SB 54-2022

Refer to Subtask

542016-832-012-001.

LR:

2,200 FC /11,100

FH

None

None

SR:

2,000 FC /

5,600 FH

Do Re-Inspection of the

LH/RH Engine Pylon

Pre-repair and Pre-SB

54-2022 Refer to

Subtask

542016-832-012-001.

None None

LR:

1,700 FC /

8,800 FH

Or

Apply the SB 54-2022. Before next flight None None

And

No crack found

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to

Subtask

542016-832-016-001.

Refer to table 2

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SERVICE BULLETIN

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

Crack found Do a Special Detailed

Inspection of the LH/RH

Engine Pylon without the

aluminium spray

protection Refer to

Subtask

542016-832-014-001.

Before next flight None None

SR:

2,000 FC /

5,600 FH

Do Re-Inspection of the

LH/RH Engine Pylon

Pre-repair and Pre-SB

54-2022 Refer to

Subtask

542016-832-012-001.

None None

LR:

1,700 FC /

8,800 FH

Or

Apply the SB 54-2022. Before next flight None None

And

No crack found after

accomplishment of

Subtask

542016-832-014-001.

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to

Subtask

542016-832-016-001.

Refer to table 2

Crack found < or =

30 mm (1.181 in.)

after embodiment of

Subtask

542016-832-014-001.

Do an Intermediate

Special Detailed

Inspection of the LH/RH

Engine Pylon Pre-repair

and Pre-SB 54-2022

Refer to Subtask

542016-832-015-001.

250 FC None None

Crack found > 30

mm (1.181 in.) after

embodiment of

Subtask

542016-832-014-001.

Contact AIRBUS Before next flight None None

Install the doubler on the

LH/RH Pylon (Refer to

Subtask

542016-833-020-001)

Before 250 FC None None

And

Crack found < or =

30 mm (1.181 in.)

after embodiment of

Subtask

542016-832-015-001.

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post repair

Refer to Subtask

542016-832-017-001.

Refer to table 3

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

Crack found > 30

mm (1.181 in.) after

embodiment of

Subtask

542016-832-015-001

is embodied)

Contact AIRBUS Before next flight None None

Table 1, Special Detailed Inspection between RIB9 and RIB10 Pre-repair and Pre-SB 54-2022 for

A310-300 aircraft.

NOTE (09): For Average Flight Time (AFT - limit between Short Range (SR) and

Long Range (LR)) configuration refer to Airworthiness Limitation Item

Document Section B.

NOTE (10): SR stands for Short Range (aircraft with an average flight time (AFT)

lower than 4 hours).

LR stands for Long Range (aircraft with an average flight time (AFT)

greater or equal than 4 hours).

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive

Interval (FC or

FH whichever

occurs first)

SR:

4,700 FC / 13,300

FH

SR:

see notes (01)

and (03)

Config. 002

After

accomplishment of

SB 54-2022.

Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to

Subtask

542016-832-016-001.

LR:

3,200 FC / 16,000

FH

LR:

see notes (02)

and (04)

None

Crack found. Contact AIRBUS Before next flight None None

SR:

see notes (01)

and (03)

SR:

9,000 FC /

25,400 FH

No crack found Do a Special Detailed

Inspection of the LH/RH

Engine Pylon Post SB

54-2022 Refer to

Subtask

542016-832-016-001.

None

LR:

see notes (02)

and (04)

LR:

7,800 FC /

39,300 FH

Table 2, Special Detailed Inspection between RIB9 and RIB10 for A310-300 aircraft Post SB 54-2022.

NOTE (01): For A310-300 aircraft with Service Bulletin No. A310-54-2022

accomplished less than 16,200 FC from Service Bulletin No.

A310-54-2022 accomplishment :

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 2,000 FC

is applicable from publication date as long as this value does not

exceed the previous figures.

NOTE (02): For A310-300 aircraft with Service Bulletin No. A310-54-2022

accomplished less than 12,900 FC from Service Bulletin No.

A310-54-2022 accomplishment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 2,000 FC

is applicable from publication date as long as this value does not

exceed the previous figures.

NOTE (03): For A310-300 aircraft with Service Bulletin No. A310-54-2022

accomplished more than 16,200 FC from Service Bulletin No.

A310-54-2022 accomplishment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 1,000 FC

is applicable from publication date as long as this value does not

exceed the previous figures.

NOTE (04): For A310-300 aircraft with Service Bulletin No. A310-54-2022

accomplished more than 12,900 FC from Service Bulletin No.

A310-54-2022 accomplishment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 1,000 FC

is applicable from publication date as long as this value does not

exceed the previous figures.

NOTE (09): For Average Flight Time (AFT - limit between Short Range (SR) and

Long Range (LR)) configuration refer to Airworthiness Limitation Item

Document Section B.

NOTE (10): SR stands for Short Range (aircraft with an average flight time (AFT)

lower than 4 hours).

LR stands for Long Range (aircraft with an average flight time (AFT)

greater or equal than 4 hours).

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

SR:

4,100 FC / 11,500

FH

SR:

see notes (05)

and (07)

Config. 002

After Installation

of the doubler on

the LH and/or RH

Pylon

Do a Special

Inspection of the

LH/RH Engine Pylon

Post repair Refer to

Subtask

542016-832-017-001.

LR:

2,700 FC / 13,900

FH

LR:

see notes (06)

and (08)

None

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

Crack found Contact AIRBUS Before next flight None None

SR:

see notes (05)

and (07)

SR:

2,400 FC / 6,900

FH

No crack found Do a Special

Inspection of the

LH/RH Engine Pylon

Post repair Refer to

Subtask

542016-832-017-001.

None

LR:

see notes (06)

and (08)

LR:

2,100 FC / 10,700

FH

Table 3, Special Detailed Inspection between RIB9 and RIB10 for A310-300 aircraft Post Repair.

NOTE (05): For A310-300 aircraft repaired less than 16,200 FC from repair

embodiment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 1,000 FC

is applicable for repaired A310-300 aircraft from publication date as

long as this value does not exceed the previous figures.

NOTE (06): For A310-300 aircraft repaired less than 13,100 FC from repair

embodiment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 1,000 FC

is applicable for repaired A310-300 aircraft from publication date as

long as this value does not exceed the previous figures.

NOTE (07): For A310-300 aircraft repaired more than 16,200 FC from repair

embodiment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 500 FC

is applicable for repaired A310-300 aircraft from publication date as

long as this value does not exceed the previous figures.

NOTE (08): For A310-300 aircraft repaired more than 13,100 FC from repair

embodiment :

- For aircraft that have already exceeded or are close to exceeding

the new or revised published values, special compliance of 500 FC

is applicable for repaired A310-300 aircraft from publication date as

long as this value does not exceed the previous figures.

NOTE (09): For Average Flight Time (AFT - limit between Short Range (SR) and

Long Range (LR)) configuration refer to Airworthiness Limitation Item

Document Section B.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 12

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SERVICE BULLETIN

NOTE (10): SR stands for Short Range (aircraft with an average flight time (AFT)

lower than 4 hours).

LR stands for Long Range (aircraft with an average flight time (AFT)

greater or equal than 4 hours).

**CONF ALL

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied 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 542016-832-801-001: Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

Get Access 0.50

On Aircraft

Do a Special Detailed Inspection of the LH/RH Engine

Pylon Pre-repair and Pre SB 54-2022.

1.00

Do a Special Detailed Inspection of the LH/RH Engine

Pylon without protection.

2.00

Do an Intermediate Special Detailed Inspection of the

LH/RH Engine Pylon Pre-repair and Pre-SB 54-2022.

1.00

Close-Up 0.50

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

NOTE: These values are valid only for one pylon.

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

Get Access 0.50

On Aircraft

Do a Special Detailed Inspection of the LH/RH Engine

Pylon Post-repair.

1.00

Close-Up 0.50

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 13

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SERVICE BULLETIN

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

NOTE: These values are valid only for one pylon.

Task 542016-832-803-001: Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

Get Access 0.50

On Aircraft

Do a Special Detailed Inspection of the LH/RH Engine

Pylon Post SB 54-2022.

1.00

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

NOTE: These values are valid only for one pylon.

Task 542016-833-802-001: Repair

Get Access 18.00

On Aircraft

Reinforce the Lower Spar with a Doubler. 8.00

Tests 3.00

Close-Up 23.00

TOTAL MANHOURS 52.00

ELAPSED TIME (HOURS) 28.00

NOTE: These values are valid only for one pylon.

**CONF 002

Task 542016-832-801-001: Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

Get Access 0.50

On Aircraft

Do a Special Detailed Inspection of the LH/RH Engine

Pylon Pre-repair and Pre SB 54-2022.

1.00

Do a Special Detailed Inspection of the LH/RH Engine

Pylon without protection.

2.00

Do an Intermediate Special Detailed Inspection of the

LH/RH Engine Pylon Pre-repair and Pre-SB 54-2022.

1.00

Close-Up 0.50

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

NOTE: These values are valid only for one pylon.

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

Get Access 0.50

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Task 542016-832-802-001: Inspection for Aircraft Post-Repair.

On Aircraft

Do a Special Detailed Inspection of the LH/RH Engine

Pylon Post-repair.

1.00

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

NOTE: These values are valid only for one pylon.

Task 542016-832-803-001: Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

Get Access 0.50

On Aircraft

Do a Special Detailed Inspection of the LH/RH Engine

Pylon Post SB 54-2022.

1.00

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

NOTE: These values are valid only for one pylon.

Task 542016-833-802-001: Repair

Get Access 18.00

On Aircraft

Reinforce the Lower Spar with a Doubler. 8.00

Tests 3.00

Close-Up 23.00

TOTAL MANHOURS 52.00

ELAPSED TIME (HOURS) 28.00

NOTE: These values are valid only for one pylon.

**CONF ALL

H. WEIGHT AND BALANCE

NOTE: If repair :

Manufacturers Empty Weight +2 KG (+4.41 LB)

Effect on Balance +47.53 KGM (+343.78 LB.FT )

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-54 20-31-00 24-00-00

24-41-00 71-00-00

Consumable Material List (CML)

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

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

Repair Instruction R54600029

Service Bulletin (SB) A310-54-2022

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-10 51-23-10 51-73-11

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-54 20-31-00 24-00-00

24-41-00 71-00-00

Consumable Material List (CML)

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

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

Repair Instruction R54600029

Service Bulletin (SB) A310-54-2022

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-10 51-23-10 51-73-11

**CONF ALL

K. PUBLICATION AFFECTED

Maintenance Planning Document (MPD) 545004-02-6

545004-02-1

545004-02-2

545004-02-3

545004-02-4

545004-02-5

Structural Repair Manual (SRM) 54-51-11

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 542016A01R02 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 by fax: +49 40 50 76 2590

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 542016A01R02

Cost 1,280.00 USD

Availability 120 calendar days from receipt of order

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

at the issue date of the Service Bulletin.

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

Kit 542016A01R02

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

NOTES

NAS1726C3E 64 Nut

NAS6703U5 28 Bolt

NAS6703U6 30 Bolt

NAS6703U6X 6 Bolt

NSA5415-40-10 1 Rivet

R5460002920200 1 Filler

R5460003020400 1 Doubler

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

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.

NOTE: Kit 542016A01R02 is valid for one pylon.

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 following tools and

equipment :

- Equipment and material for control by Eddy current as per NTM 54-50-40 Page

Block 601.

or

- Equipment and material for liquid penetrant inspection as per NTM 54-50-40 Page

Block 901.

(3) Special Tools

None

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 18

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 542016-832-801-001 - Inspection for Aircraft Pre Service Bulletin No. A310-54-2022 and

pre-repair.

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.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

Task Associated Data

**CONF 001

Zone

410 420

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

**CONF 002

Zone

410 420

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 542016-910-001-001 - 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

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with:

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 542016-910-001-001 - 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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 20

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with:

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 542016-941-001-001 - 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

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) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

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

(d) Remove the access doors (Refer to AMM 06-41-54 Page Block 001) :

1 RH pylon: 425AL, 426AR.

2 LH pylon: 415AL, 416AR.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

**CONF 002

(1) Subtask 542016-941-001-001 - 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

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) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

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

(d) Remove the access doors (Refer to AMM 06-41-54 Page Block 001) :

1 RH pylon: 425AL, 426AR.

2 LH pylon: 415AL, 416AR.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 542016-832-012-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon Pre-repair and Pre SB 54-2022.

Work Zones and Access Panels

Zone Access/Work location

410 Work location from Rib 9 to Rib 10

420 Work location from Rib 9 to Rib 10

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, Page Block 601

54-50-40, Page Block 901

Service Bulletin (SB) A310-54-2022

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 22

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SERVICE BULLETIN

References

Fig. A-FBAAA

Areas to Be Inspected Pre Repair and

Pre SB 54-2022

Sheet 01

Fig. A-FBBAA

Areas to Be Inspected Post Repair

Sheet 01

(a) From the inside, on LH and RH pylons, do a special detailed Eddy Current

Inspection (Refer to NTM 54-50-40 Page Block 601) or Liquid Penetrant Inspection

(Refer to NTM 54-50-40 Page Block 901) in the lower spar axis between ribs 9 and

10.

Refer to Fig. A-FBAAA Sheet 01

1 If a crack is found :

- Refer to SUBTASK 542016-832-014 001 Do a Special Detailed Inspection

of the LH/RH Engine Pylon without protection.

2 If no crack is found :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Re-inspect the area as described in SUBTASK 542016-832-012 001 Do

a Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair and

Pre SB 54-2022. at the interval given in Planning Information Paragraph

E.(2).

or

Accomplish Service Bulletin No. A310-54-2022 and apply SUBTASK

542016-832-016 001 Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post SB 54-2022. at the threshold given in Planning

Information Paragraph E.(2).

(2) Subtask 542016-832-014-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon without protection.

Work Zones and Access Panels

Zone Access/Work location

410

420

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON DESTRUCTIVE

TESTING

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

References

Non Destructive Test Manual (NTM) 54-50-40, Page Block 601

54-50-40, Page Block 901

Service Bulletin (SB) A310-54-2022

Structural Repair Manual (SRM) 51-21-10

51-23-10

51-73-11

Fig. A-FBAAA

Areas to Be Inspected Pre Repair and

Pre SB 54-2022

Sheet 01

(a) Smooth blend out the area to remove the aluminium spray protection or cadmium

plating protection 0.17 mm (0.007 in.) (Refer to SRM 51-73-11).

(b) From the inside, on LH and RH pylon, do an Eddy Current re-Inspection (Refer to

NTM 54-50-40, Page Block 601) and Liquid Penetrant Inspection (Refer to NTM

54-50-40, Page Block 901) in the lower spar axis between ribs 9 and 10.

Refer to Fig. A-FBAAA Sheet 01

1 If no crack is found :

a Re-protect the area by pad cadmium plating (Refer to SRM 51-21-10)

and apply the paint coating (Refer to SRM 51-23-10).

b Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

c Re-inspect the area as described in SUBTASK 542016-832-012 001 Do

a Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair and

Pre SB 54-2022. at the interval given in Planning Information Paragraph

E.(2).

or

Accomplish Service Bulletin No. A310-54-2022 and apply SUBTASK

542016-832-016 001 Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post SB 54-2022. at the thresholds given in Planning

Information Paragraph E.(2).

2 If crack is found =< 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Do an intermediate inspection as described in SUBTASK

542016-832-015 001 Do an Intermediate Special Detailed Inspection of

the LH/RH Engine Pylon Pre-repair and Pre-SB 54-2022. at 250FC.

3 If crack is found > 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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b Contact Airbus before next flight.

(3) Subtask 542016-832-015-001 - Do an Intermediate Special Detailed Inspection of

the LH/RH Engine Pylon Pre-repair and Pre-SB 54-2022.

Work Zones and Access Panels

Zone Access/Work location

410

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, Page Block 601

54-50-40, Page Block 901

Structural Repair Manual (SRM) 51-21-10

51-23-10

Fig. A-FBAAA

Areas to Be Inspected Pre Repair and

Pre SB 54-2022

Sheet 01

(a) From the inside, on LH and RH pylon, do an Eddy Current re-Inspection (Refer to

NTM 54-50-40, Page Block 601) or Liquid Penetrant Inspection (Refer to NTM

54-50-40, Page Block 901) in the lower spar axis between ribs 9 and 10.

Refer to Fig. A-FBAAA Sheet 01

1 If crack is > 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact Airbus before next flight.

2 If crack is =< 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Do the repair before 250 FC as described in TASK 542016-833-802 001

Repair and inspect as described in SUBTASK 542016-832-017 001 Do a

Special Detailed Inspection of the LH/RH Engine Pylon Post-repair.

c Re-protect the area by pad cadmium plating (Refer to SRM 51-21-10)

and apply the paint coating (Refer to SRM 51-23-10).

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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**CONF 002

(1) Subtask 542016-832-012-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon Pre-repair and Pre SB 54-2022.

Work Zones and Access Panels

Zone Access/Work location

410 Work location from Rib 9 to Rib 10

420 Work location from Rib 9 to Rib 10

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, Page Block 601

54-50-40, Page Block 901

Service Bulletin (SB) A310-54-2022

Fig. A-FBAAA

Areas to Be Inspected Pre Repair and

Pre SB 54-2022

Sheet 01

Fig. A-FBBAA

Areas to Be Inspected Post Repair

Sheet 01

(a) From the inside, on LH and RH pylons, do a special detailed Eddy Current

Inspection (Refer to NTM 54-50-40 Page Block 601) or Liquid Penetrant Inspection

(Refer to NTM 54-50-40 Page Block 901) in the lower spar axis between ribs 9 and

10.

Refer to Fig. A-FBAAA Sheet 01

1 If a crack is found :

- Refer to SUBTASK 542016-832-014 001 Do a Special Detailed Inspection

of the LH/RH Engine Pylon without protection.

2 If no crack is found :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Re-inspect the area as described in SUBTASK 542016-832-012 001 Do

a Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair and

Pre SB 54-2022. at the interval given in Planning Information Paragraph

E.(2).

or

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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Accomplish Service Bulletin No. A310-54-2022 and apply SUBTASK

542016-832-016 001 Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post SB 54-2022. at the threshold given in Planning

Information Paragraph E.(2).

(2) Subtask 542016-832-014-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon without protection.

Work Zones and Access Panels

Zone Access/Work location

410

420

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 54-50-40, Page Block 601

54-50-40, Page Block 901

Service Bulletin (SB) A310-54-2022

Structural Repair Manual (SRM) 51-21-10

51-23-10

51-73-11

Fig. A-FBAAA

Areas to Be Inspected Pre Repair and

Pre SB 54-2022

Sheet 01

(a) Smooth blend out the area to remove the aluminium spray protection or cadmium

plating protection 0.17 mm (0.007 in.) (Refer to SRM 51-73-11).

(b) From the inside, on LH and RH pylon, do an Eddy Current re-Inspection (Refer to

NTM 54-50-40, Page Block 601) and Liquid Penetrant Inspection (Refer to NTM

54-50-40, Page Block 901) in the lower spar axis between ribs 9 and 10.

Refer to Fig. A-FBAAA Sheet 01

1 If no crack is found :

a Re-protect the area by pad cadmium plating (Refer to SRM 51-21-10)

and apply the paint coating (Refer to SRM 51-23-10).

b Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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c Re-inspect the area as described in SUBTASK 542016-832-012 001 Do

a Special Detailed Inspection of the LH/RH Engine Pylon Pre-repair and

Pre SB 54-2022. at the interval given in Planning Information Paragraph

E.(2).

or

Accomplish Service Bulletin No. A310-54-2022 and apply SUBTASK

542016-832-016 001 Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post SB 54-2022. at the thresholds given in Planning

Information Paragraph E.(2).

2 If crack is found =< 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Do an intermediate inspection as described in SUBTASK

542016-832-015 001 Do an Intermediate Special Detailed Inspection of

the LH/RH Engine Pylon Pre-repair and Pre-SB 54-2022. at 250FC.

3 If crack is found > 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact Airbus before next flight.

(3) Subtask 542016-832-015-001 - Do an Intermediate Special Detailed Inspection of

the LH/RH Engine Pylon Pre-repair and Pre-SB 54-2022.

Work Zones and Access Panels

Zone Access/Work location

410

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, Page Block 601

54-50-40, Page Block 901

Structural Repair Manual (SRM) 51-21-10

51-23-10

Fig. A-FBAAA

Areas to Be Inspected Pre Repair and

Pre SB 54-2022

Sheet 01

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 28

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(a) From the inside, on LH and RH pylon, do an Eddy Current re-Inspection (Refer to

NTM 54-50-40, Page Block 601) or Liquid Penetrant Inspection (Refer to NTM

54-50-40, Page Block 901) in the lower spar axis between ribs 9 and 10.

Refer to Fig. A-FBAAA Sheet 01

1 If crack is > 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact Airbus before next flight.

2 If crack is =< 30mm (1.181 in.):

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Do the repair before 250 FC as described in TASK 542016-833-802 001

Repair and inspect as described in SUBTASK 542016-832-017 001 Do a

Special Detailed Inspection of the LH/RH Engine Pylon Post-repair.

c Re-protect the area by pad cadmium plating (Refer to SRM 51-21-10)

and apply the paint coating (Refer to SRM 51-23-10).

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 542016-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

71-00-00, Page Block 401

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 29

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

equipment.

(b) Install the access doors (Refer to AMM 06-41-54, Page Block 001):

1 RH pylon : 425AL, 426AR.

2 LH pylon : 415AL, 416AR.

(c) Remove the access platform(s).

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

**CONF 002

(1) Subtask 542016-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

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 access doors (Refer to AMM 06-41-54, Page Block 001):

1 RH pylon : 425AL, 426AR.

2 LH pylon : 415AL, 416AR.

(c) Remove the access platform(s).

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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 30

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SERVICE BULLETIN

Task 542016-832-802-001 - Inspection for Aircraft Post-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.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

Task Associated Data

**CONF 001

Zone

410 420

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

**CONF 002

Zone

410 420

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 31

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**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 542016-910-005-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

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

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with:

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-839-004-001 - 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 542016-910-005-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 32

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with:

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-839-004-001 - 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 542016-941-005-001 - 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

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) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

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

(d) Remove the access doors (Refer to AMM 06-41-54 Page Block 001) :

1 RH pylon: 425AL, 426AR.

2 LH pylon: 415AL, 416AR.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 33

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SERVICE BULLETIN

**CONF 002

(1) Subtask 542016-941-005-001 - 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

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) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

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

(d) Remove the access doors (Refer to AMM 06-41-54 Page Block 001) :

1 RH pylon: 425AL, 426AR.

2 LH pylon: 415AL, 416AR.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 542016-832-017-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post-repair.

Work Zones and Access Panels

Zone Access/Work location

410

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, Page Block 601

54-50-40, Page Block 901

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 34

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References

Fig. A-FBBAA

Areas to Be Inspected Post Repair

Sheet 01

(a) From the inside, on LH and RH pylons , do a special detailed Eddy Current

Inspection (Refer to NTM 54-50-40 Page Block 601) or Liquid Penetrant Inspection

(Refer to NTM 54-50-40 Page Block 901) in the lower spar axis between ribs 9 and

10 at the threshold given in Planning Information Paragraph E.(2).

Refer to Fig. A-FBBAA Sheet 01.

1 If no crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Re-inspect the area as described in SUBTASK 542016-832-017 001 Do

a Special Detailed Inspection of the LH/RH Engine Pylon Post-repair. at

the interval given in Planning Information Paragraph E.(2).

2 If a crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact AIRBUS before next flight.

**CONF 002

(1) Subtask 542016-832-017-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post-repair.

Work Zones and Access Panels

Zone Access/Work location

410

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, Page Block 601

54-50-40, Page Block 901

Fig. A-FBBAA

Areas to Be Inspected Post Repair

Sheet 01

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 35

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SERVICE BULLETIN

(a) From the inside, on LH and RH pylons , do a special detailed Eddy Current

Inspection (Refer to NTM 54-50-40 Page Block 601) or Liquid Penetrant Inspection

(Refer to NTM 54-50-40 Page Block 901) in the lower spar axis between ribs 9 and

10 at the threshold given in Planning Information Paragraph E.(2).

Refer to Fig. A-FBBAA Sheet 01.

1 If no crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Re-inspect the area as described in SUBTASK 542016-832-017 001 Do

a Special Detailed Inspection of the LH/RH Engine Pylon Post-repair. at

the interval given in Planning Information Paragraph E.(2).

2 If a crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact AIRBUS before next flight.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 542016-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

71-00-00, Page Block 401

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

equipment.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 36

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(b) Install the access doors (Refer to AMM 06-41-54, Page Block 001) :

1 RH pylon : 425AL, 426AR.

2 LH pylon : 415AL, 416AR.

(c) Remove the access platform(s).

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

**CONF 002

(1) Subtask 542016-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

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 access doors (Refer to AMM 06-41-54, Page Block 001) :

1 RH pylon : 425AL, 426AR.

2 LH pylon : 415AL, 416AR.

(c) Remove the access platform(s).

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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 37

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This Page Intentionally Left Blank

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 38

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Task 542016-832-803-001 - Inspection for Aircraft Post Service Bulletin No. A310-54-2022.

**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.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

Task Associated Data

**CONF 001

Zone

410 420

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

**CONF 002

Zone

410 420

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 39

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SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 542016-941-007-001 - Job Set-up

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

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with:

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-839-005-001 - 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 542016-941-007-001 - Job Set-up

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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 40

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with:

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-839-005-001 - 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 542016-941-006-001 - 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

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) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

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

(d) Remove the access doors (Refer to AMM 06-41-54 Page Block 001) :

1 RH pylon: 425AL, 426AR.

2 LH pylon: 415AL, 416AR.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 41

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SERVICE BULLETIN

**CONF 002

(1) Subtask 542016-941-006-001 - 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

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) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

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

(d) Remove the access doors (Refer to AMM 06-41-54 Page Block 001) :

1 RH pylon: 425AL, 426AR.

2 LH pylon: 415AL, 416AR.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 542016-832-016-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post SB 54-2022.

Work Zones and Access Panels

Zone Access/Work location

410 Work location from Rib 9 to Rib 10

420 Work location from Rib 9 to Rib 10

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, Page Block 601

54-50-40, Page Block 901

Service Bulletin (SB) A310-54-2022

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 42

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SERVICE BULLETIN

References

Fig. A-FBCAA

Areas to Be Inspected Post SB 54-2022

Sheet 01

(a) From the inside, on LH and RH pylons , do a special detailed Eddy Current

Inspection (Refer to NTM 54-50-40 Page Block 601) or Liquid Penetrant Inspection

(Refer to NTM 54-50-40 Page Block 901) in the lower spar axis between ribs 9 and

10 at the threshold given in Planning Information Paragraph E.(2).

Refer to Fig. A-FBCAA Sheet 01.

1 If no crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Re-inspect the area as described inSUBTASK 542016-832-016 001 Do a

Special Detailed Inspection of the LH/RH Engine Pylon Post SB 54-2022.

at the interval given in Planning Information Paragraph E.(2).

2 If a crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact AIRBUS before next flight.

**CONF 002

(1) Subtask 542016-832-016-001 - Do a Special Detailed Inspection of the LH/RH

Engine Pylon Post SB 54-2022.

Work Zones and Access Panels

Zone Access/Work location

410 Work location from Rib 9 to Rib 10

420 Work location from Rib 9 to Rib 10

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, Page Block 601

54-50-40, Page Block 901

Service Bulletin (SB) A310-54-2022

Fig. A-FBCAA

Areas to Be Inspected Post SB 54-2022

Sheet 01

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

(a) From the inside, on LH and RH pylons , do a special detailed Eddy Current

Inspection (Refer to NTM 54-50-40 Page Block 601) or Liquid Penetrant Inspection

(Refer to NTM 54-50-40 Page Block 901) in the lower spar axis between ribs 9 and

10 at the threshold given in Planning Information Paragraph E.(2).

Refer to Fig. A-FBCAA Sheet 01.

1 If no crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Re-inspect the area as described inSUBTASK 542016-832-016 001 Do a

Special Detailed Inspection of the LH/RH Engine Pylon Post SB 54-2022.

at the interval given in Planning Information Paragraph E.(2).

2 If a crack is detected :

a Send to AIRBUS inspection report, refer to Appendix 01: Inspection

Report

b Contact AIRBUS before next flight.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 542016-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

71-00-00, Page Block 401

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

equipment.

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 44

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SERVICE BULLETIN

(b) Install the access doors (Refer to AMM 06-41-54, Page Block 001) :

1 RH pylon : 425AL, 426AR.

2 LH pylon : 415AL, 416AR.

(c) Remove the access platform(s).

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

**CONF 002

(1) Subtask 542016-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

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 access doors (Refer to AMM 06-41-54, Page Block 001) :

1 RH pylon : 425AL, 426AR.

2 LH pylon : 415AL, 416AR.

(c) Remove the access platform(s).

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

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 45

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SERVICE BULLETIN

Task 542016-833-802-001 - 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.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 52.00

ELAPSED TIME (HOURS) 28.00

**CONF 002

Manpower

TOTAL MANHOURS 52.00

ELAPSED TIME (HOURS) 28.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 542016-910-002-001

Manpower Resources

Skills NON SPECIFIC

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 47

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SERVICE BULLETIN

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

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with :

Solvent General

Purpose

11-026 As required

(2) Subtask 542016-900-016-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 542016-910-002-001

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

References

Aircraft Maintenance Manual (AMM) 20-31-00

Consumable Material List (CML)

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

(b) Clean the surfaces to seal (Refer to AMM 20-31-00) with :

Solvent General

Purpose

11-026 As required

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

(2) Subtask 542016-900-016-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 542016-941-008-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Remove the power plant (Refer to AMM 71-00-00 Page Block 401).

**CONF 002

(1) Subtask 542016-941-008-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Remove the power plant (Refer to AMM 71-00-00 Page Block 401).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 542016-833-020-001 - Reinforce the Lower Spar with a Doubler.

Manpower Resources

Manhours 8.00

Minimum number of person 1

Subtask elapsed time 8.00

Skills AIRFRAME

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Material necessary to do the job

Kit 542016A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NAS1726C3E 64 Nut

NAS6703U5 28 Bolt

NAS6703U6 30 Bolt

NAS6703U6X 6 Bolt

NSA5415-40-10 1 Rivet

R5460002920200 1 Filler

R5460003020400 1 Doubler

NOTE: Kit 542016A01R02 is valid for one pylon.

References

Repair Instruction R54600029

NOTE: Description below is given for one pylon.

(a) Reinforce the lower spar with a doubler.

Refer to Kit 542016A01R02

Refer to Repair Instruction R54600029

1 Install :

1 Doubler R5460003020400

1 Filler R5460002920200

with :

64 Nut NAS1726C3E

28 Bolt NAS6703U5

30 Bolt NAS6703U6

6 Bolt NAS6703U6X

1 Rivet NSA5415-40-10

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

**CONF 002

(1) Subtask 542016-833-020-001 - Reinforce the Lower Spar with a Doubler.

Manpower Resources

Manhours 8.00

Minimum number of person 1

Subtask elapsed time 8.00

Skills AIRFRAME

Material necessary to do the job

Kit 542016A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NAS1726C3E 64 Nut

NAS6703U5 28 Bolt

NAS6703U6 30 Bolt

NAS6703U6X 6 Bolt

NSA5415-40-10 1 Rivet

R5460002920200 1 Filler

R5460003020400 1 Doubler

NOTE: Kit 542016A01R02 is valid for one pylon.

References

Repair Instruction R54600029

NOTE: Description below is given for one pylon.

(a) Reinforce the lower spar with a doubler.

Refer to Kit 542016A01R02

Refer to Repair Instruction R54600029

1 Install :

1 Doubler R5460003020400

1 Filler R5460002920200

with :

64 Nut NAS1726C3E

28 Bolt NAS6703U5

30 Bolt NAS6703U6

6 Bolt NAS6703U6X

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 51

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SERVICE BULLETIN

1 Rivet NSA5415-40-10

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 542016-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

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

NOTE: Install the power plant (Refer to SUBTASK 542016-942-002 001 Closeup ) before accomplishment of the test below.

(a) Do the test after removal/installation of the power plant (Refer to AMM 71-00-00

Page Block 401).

**CONF 002

(1) Subtask 542016-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

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

NOTE: Install the power plant (Refer to SUBTASK 542016-942-002 001 Closeup ) before accomplishment of the test below.

(a) Do the test after removal/installation of the power plant (Refer to AMM 71-00-00

Page Block 401).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 542016-942-002-001 - Close-up

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

References

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

NOTE: Install the power plant before accomplishment of the test (Refer to

SUBTASK 542016-700-001 001 Testing ).

(a) Install the power plant (Refer to AMM 71-00-00 Page Block 401).

**CONF 002

(1) Subtask 542016-942-002-001 - Close-up

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

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

NOTE: Install the power plant before accomplishment of the test (Refer to

SUBTASK 542016-700-001 001 Testing ).

(a) Install the power plant (Refer to AMM 71-00-00 Page Block 401).

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 53

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SERVICE BULLETIN

**CONF ALL

A

B

A

A

AREAS TO BE INSPECTED

B RIB 18

RIB 12

RIB 10

RIB 9

RIB 8

LOWER SPAR

RIB 8 RIB 9 RIB 10

B_SB_542016_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Areas to Be Inspected Pre Repair and Pre SB 54-2022

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 54

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SERVICE BULLETIN

**CONF ALL

CENTER

STIFFENER

B

AREAS TO BE INSPECTED

RIB 9 RIB 10

A

A

A B RIB 18

RIB 12

RIB 10

RIB 9

RIB 8

LOWER SPAR

B_SB_542016_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Areas to Be Inspected Post Repair

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 55

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SERVICE BULLETIN

**CONF ALL

A

B

A

A

AREAS TO BE INSPECTED

B RIB 18

RIB 12

RIB 10

RIB 9

RIB 8

LOWER SPAR

RIB 8 RIB 9 RIB 10

B_SB_542016_5_BCAA_01_00

Figure A-FBCAA - Sheet 01

Areas to Be Inspected Post SB 54-2022

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 56

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SERVICE BULLETIN

**CONF ALL

QUESTION

FINDING

ACTION

OR

CRACK FINDING NO

FROM THE INSIDE, DO A SPECIAL DETAILED EDDY CURRENT INSPECTION OR

LIQUID PENETRANT INSPECTION (REFER TO SUBTASK 542016−832−012−001)

IN THE LOWER SPAR AXIS BETWEEN RIBS 9 AND 10

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

YES

YES CRACK FINDING NO

DO A SPECIAL DETAILED EDDY CURRENT INSPECTION

AND LIQUID PENETRANT INSPECTION

(REFER TO SUBTASK 542016−832−014−001)

YES CRACK FINDING NO

CONTACT AIRBUS

BEFORE NEXT FLIGHT

CRACK 30 mm

(1.181 in)

CRACK 30 mm

(1.181 in)

DO A SPECIAL DETAILED EDDY CURRENT INSPECTION OR LIQUID 

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

PENETRANT INSPECTION (REFER TO SUBTASK 542016−832−017−001) 

RE−INSPECT BY A SPECIAL DETAILED EDDY CURRENT INSPECTION OR LIQUID

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

PENETRANT INSPECTION (REFER TO SUBTASK 542016−832−017−001) 

YES NO

REPAIR BEFORE 250 FC

(REFER TO SUBTASK 542016−833−020−001)

DO AN INTERMEDIATE SPECIAL DETAILED EDDY CURRENT

INSPECTION OR LIQUID PENETRANT INSPECTION

(REFER TO SUBTASK 542016−832−015−001) AT 250 FC

CRACK 30 mm

(1.181 in)

OR

APPLY SERVICE BULLETIN

No. A310−54−2022 (10328S20412) EDDY CURRENT INSPECTION

OR LIQUID PENETRANT INSPECTION

AT THE INTERVAL GIVEN IN

PLANNING INFORMATION PARAGRAPH E.(2)

(REFER TO SUBTASK 542016−832−012−001)

RE−INSPECT BY A SPECIAL DETAILED

DO A SPECIAL DETAILED EDDY CURRENT

INSPECTION OR LIQUID PENETRANT INSPECTION

AT THE THRESHOLD GIVEN IN

PLANNING INFORMATION PARAGRAPH E.(2)

(REFER TO SUBTASK 542016−832−016−001)

CRACK FINDING

CONTACT AIRBUS

BEFORE NEXT

YES NO

EDDY CURRENT INSPECTION

OR LIQUID PENETRANT INSPECTION

AT THE INTERVAL GIVEN IN

PLANNING INFORMATION PARAGRAPH E.(2)

(REFER TO SUBTASK 542016−832−016−001)

RE−INSPECT BY A SPECIAL DETAILED

FLIGHT

B_SB_542016_5_FAAA_01_03

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 57

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This Page Intentionally Left Blank

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Appendix 01: Inspection Report

**CONF ALL

(1) Appendix 01: Inspection Report

The results 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.: A310-54-2016

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SERVICE BULLETIN

Appendix 01: Inspection Report

**CONF ALL

AREA 1 AREA 2

CENTER

STIFFENER

AREA 1 OR 2

DEPTH

PLEASE PRECISE OTHER FINDINGS THAN CRACK :

NO CRACK

CRACK

LENGTH DEPTH

PYLON

LEFT

PYLON

RIGHT

AREA 1

AREA 2

AREA 1

AREA 2

RIB 9 RIB 10

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A310−54−2016

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX SRTUCTURE − ENGINE PYLON

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 36 14 EDDY CURRENT

LIQUID PENETRANT

LENGTH

EXAMPLE OF CRACK DIMENSIONS SHOWN

B_SB_542016_5_RAAA_01_01

Figure A-FRAAA - Sheet 01

Inspection Report for Aircraft Pre-repair and Pre-SB 54-2022

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 2

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SERVICE BULLETIN

Appendix 01: Inspection Report

**CONF ALL

NO CRACK

CRACK

LENGTH DEPTH

PYLON

LEFT

PYLON

RIGHT

AREA 1

AREA 2

AREA 1

AREA 2

AREA 2

CENTER

STIFFENER

AFTER REPAIR IN ACCORDANCE

WITH DRAWING R54600029 YES NO

AREA 1

RIB 9 RIB 10

DEPTH

PLEASE PRECISE OTHER FINDINGS THAN CRACK :

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A310−54−2016

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : EDDY CURRENT

LIQUID PENETRANT

LENGTH

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX SRTUCTURE − ENGINE PYLON

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 36 14

AREA 1 OR 2

EXAMPLE OF CRACK DIMENSIONS SHOWN

B_SB_542016_5_RBAA_01_01

Figure A-FRBAA - Sheet 01

Inspection Report for Aircraft Post-repair

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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SERVICE BULLETIN

Appendix 01: Inspection Report

**CONF ALL

AREA 1 AREA 2

CENTER

STIFFENER

DEPTH

PLEASE PRECISE OTHER FINDINGS THAN CRACK :

NO CRACK

CRACK

LENGTH DEPTH

PYLON

LEFT

PYLON

RIGHT

AREA 1

AREA 2

AREA 1

AREA 2

RIB 9 RIB 10

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A310−54−2016

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX SRTUCTURE − ENGINE PYLON

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 36 14 EDDY CURRENT

LIQUID PENETRANT

LENGTH

YES NO AFTER ACCOMPLISHMENT OF

SERVICE BULLETIN No. A310−54−2022

AREA 1 OR 2

EXAMPLE OF CRACK DIMENSIONS SHOWN

B_SB_542016_5_RCAA_01_01

Figure A-FRCAA - Sheet 01

Inspection Report for Aircraft Post-SB 54-2022

DATE: Nov 12/91 SERVICE BULLETIN No.: A310-54-2016

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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.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 1

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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.: A310-54-2016

REVISION No.: 06 - Jan 16/13 Page: 1

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