@A318/A319/A320/A321

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: 71

TITLE: POWER PLANT - GENERAL - FORWARD MOUNT - INSPECTION OF

FORWARD ENGINE MOUNT

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A320-71-1064

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 01 issued to make compliance MANDATORY following the issue of AD No. 2015-0004.

Also this revision adds reference to AMM Tasks 71-00-20-000-802 and 71-00-20-400-802 in paragraph

C. Procedure.

CHANGES

The main changes of the revision are:

- Compliance becomes MANDATORY,

- AD No. 2015-0004 added in References/Repercussions,

- Table 1 added in Accomplishment Timescale,

- AMM Tasks 71-00-20-000-802 and 71-00-20-400-802 added in paragraph C. Procedure.

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

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REVISION TRANSMITTAL SHEET

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

REASON

Advantages ADVANTAGES UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 711064- 832-801-001-Inspection of

the Serial Number (SN) of the Forward

Engine Mount Crossbeam Attach Pin for

Engines 1 and 2 in accordance with VSB

Subtask 711064-832-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Fig. A-FFAAA

Fig. A-FFAAA Sheet 01 SHEET UPDATED R

FILING 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

No previous revision

REVISION SEQUENCE

ORIGINAL: Nov 05/14

REVISION No. : 01 - Apr 01/15

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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: 71

TITLE: POWER PLANT - GENERAL - FORWARD MOUNT - INSPECTION OF

FORWARD ENGINE MOUNT

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Manufacturing metallurgical discontinuities have been reported on one identified batch of forward engine

mount crossbeam attach pins PN 740-2022-501 fitted on A320 aircraft family powered by IAE V2500

Engine.

Investigations concluded this defect could generate a stress concentration leading to an adverse effect

on the fatigue life, therefore all identified attach pins manufactured from the discrepant raw material are

subject to replacement.

This Inspection Service Bulletin is published to advise all operators of A320 aicraft powered by IAE

V2500 Engines of the issue of UTAS Service Bulletin No. V2500-NAC-71-0323.

This Inspection Service Bulletin provides instructions for a onetime detailed visual inspection to check

the serial number (SN) of the forward engine mount crossbeam to main beam attach pins P/N

740-2022-501 and to remove and replace the affected attach pins which are listed in the VSB.

Accomplishment of this Inspection Service Bulletin will enable the replacement of the affected attach

pins and thus restoring the part structural design objective.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

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SUMMARY

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

AWC BAW CBJ CCA CES CHB CSC CSN CSZ DLH HVN IGO IYE

JSA QTR TAM THY TTW VOI WZZ

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER Airworthiness Directive No. 2015-0004

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 711064-832-801-001: Inspection of the Serial Number (SN) of the Forward Engine Mount

Crossbeam Attach Pin for Engines 1 and 2 in accordance with VSB

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

Inspect the Serial Number (SN) of the Forward Engine

Mount Crossbeam Attach Pin for Engines 1 and 2 in

accordance with VSB

UTAS Service Bulletin No. V2500-

NAC-71-0323

APPENDICES

Appendix 01: Elapsed Time Assumption

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SUMMARY

**CONF ALL

B

Z400

Z400

A

A

RH SHOWN

LH SYMMETRICAL

NOTE:

INSPECTION AREA 

A

B

ATTACH PIN UNDER THE RETAINERS

N_SB_711064_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

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SUMMARY

This Page Intentionally Left Blank

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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: 71

TITLE: POWER PLANT - GENERAL - FORWARD MOUNT - INSPECTION OF

FORWARD ENGINE MOUNT

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

319-132 319-133 320-232 320-233 321-231 321-232

(2) Effectivity by MSN

4593 4602 4620 4637-4638 4642-4644 4660 4677 4690 4696 4700-4701 4703

4706-4707 4710 4716 4719 4725-4726 4731 4736-4737 4741 4746 4751-4755 4757

4761-4762 4772-4775 4779 4782-4784 4786 4788 4790-4791 4798 4804 4813

(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

AWC 4701

BAW 4725 4791

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OPERATOR MSN

CBJ 4602 4677

CCA 4593 4719 4775

CES 4638 4746

CHB 4644

CSC 4642 4660 4707 4731

CSN 4696 4751 4782

CSZ 4620 4726

DLH 4710 4753

HVN 4703 4737 4783

IGO 4637 4752 4757 4762 4813

IYE 4690

JSA 4772 4786

QTR 4700 4754 4784

TAM 4773

THY 4643 4706 4755 4761 4774 4779 4788 4790

TTW 4804

VOI 4741 4798

WZZ 4716 4736

(4) Configuration by MSN

MSN CONFIGURATION

4593 4602 4620 4637 4638 4642 4643 4644 4660 4677 4690

4696 4700 4701 4703 4706 4707 4710 4716 4719 4725 4726

4731 4736 4737 4741 4746 4751 4752 4753 4754 4755 4757

4761 4762 4772 4773 4774 4775 4779 4782 4783 4784 4786

4788 4790 4791 4798 4804 4813

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

None

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Manufacturing metallurgical discontinuities have been reported on one identified batch of

forward engine mount crossbeam attach pins PN 740-2022-501 fitted on A320 aircraft

family powered by IAE V2500 Engine.

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Investigations concluded this defect could generate a stress concentration leading to an

adverse effect on the fatigue life, therefore all identified attach pins manufactured from

the discrepant raw material are subject to replacement.

(2) Objective/Action

This Inspection Service Bulletin is published to advise all operators of A320 aicraft

powered by IAE V2500 Engines of the issue of UTAS Service Bulletin No. V2500-

NAC-71-0323.

This Inspection Service Bulletin provides instructions for a onetime detailed visual

inspection to check the serial number (SN) of the forward engine mount crossbeam to

main beam attach pins P/N 740-2022-501 and to remove and replace the affected attach

pins which are listed in the VSB.

(3) Advantages

Accomplishment of this Inspection Service Bulletin will enable the replacement of the

affected attach pins and thus restoring the part structural design objective.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 711064-832-801-001: Inspection of the Serial Number (SN) of the Forward Engine

Mount Crossbeam Attach Pin for Engines 1 and 2 in accordance with VSB

(1) Inspect the Serial Number (SN) of the Forward Engine Mount Crossbeam Attach Pin

for Engines 1 and 2 in accordance with VSB

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.

Table 1, Config. 001 - Inspection of the Serial Number (SN) of the forward engine mount crossbeam

attach pin for the Engines 1 and 2

Compliance time (whichever occurs

later)

Condition Action

Threshold

(whichever occurs

first)

Grace period

(whichever occurs

first)

Repetitive

interval

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Table 1, Config. 001 - Inspection of the Serial Number (SN) of the forward engine mount crossbeam

attach pin for the Engines 1 and 2

All aircraft Do an inspection of

the engine mount

crossbeam pin

Serial Number (SN)

for the Engine 1 and

2, in accordance

with Task

711064-832-801-001

Within 24 months,

or at the next

engine removal, or

within 7500 flight

hours or 5000 flight

cycles after the

effective date of

Airworthiness

Directive No.

2015-0004

None None

Remove and replace

the affected attach

pin on the Engine 1

and/ or Engine 2 in

accordance with

substask

711064-832-001-001

The pin SN is Before next flight None None

found listed in the

VSB

Send the inspection

report to Airbus

None None None

Check the engine

maintenance records

to verify the current

location of the

affected pin

The pin SN is not None None None

found listed in the

VSB, if the engine

replaced since at

the first flight

Send the inspection

report to Airbus

None None None

The pin SN is not

found listed in the

VSB, if the engine

not removed since

at the first flight

Contact Airbus and

follow their

instructions

None None None

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.

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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.

Task 711064-832-801-001: Inspection of the Serial Number (SN) of the Forward Engine Mount

Crossbeam Attach Pin for Engines 1 and 2 in accordance with VSB

Get Access 1.00

Close-Up 1.00

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

Inspect the Serial Number (SN) of the Forward Engine

Mount Crossbeam Attach Pin for Engines 1 and 2 in

accordance with VSB

UTAS Service Bulletin No. V2500-

NAC-71-0323

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumption.

NOTE: The minimum manhours necessary to accomplish this Service Bulletin are

those for the Inspection. Depending on the inspection result, additional

manhours can apply.

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Airworthiness Directive (AD) Airworthiness Directive No.

2015-0004

Aircraft Maintenance Manual (AMM) 06-20-00 12-34-24 71-00-20

71-13-00 78-30-00 78-32-00

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

Vendor Service Bulletin (VSB) UTAS Service Bulletin No. V2500-

NAC-71-0323

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

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M. SPARES

Fwd Eng Attach Pin 740-2022-501

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated direcly with UTAS as per

instructions given in UTAS Service Bulletin No. V2500-NAC-71-0323.

(2) Price and Availability

No AIRBUS Kit will be provided.

Refer to UTAS Service Bulletin No. V2500-NAC-71-0323 for the equipment modification

sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to UTAS Service Bulletin No. V2500-NAC-71-0323 for the industry support terms of the

Vendor Service Bulletin parts and labor.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

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 the

subsequent referenced AMM tasks:

- AMM Task 71-00-20-000-802

(3) Special Tools

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 711064-832-801-001 - Inspection of the Serial Number (SN) of the Forward Engine

Mount Crossbeam Attach Pin for Engines 1 and 2 in accordance with VSB

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 accomplishment instructions of this service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

"refer to" are used and the operator has a procedure accepted by the local

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition

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.

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Task Associated Data

Zone

430 440

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

UTAS Service Bulletin No. V2500-NAC-71-0323

A. GENERAL

(1) Subtask 711064-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

(a) For the identification of Zones, refer to AMM 06-20-00, Page Block 001.

(b) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(2) Subtask 711064-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 711064-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

Task 71-13-00-010-010

Task 78-30-00-040-012

Task 78-32-00-010-010

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

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- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin available

- All the circuit breakers are in closed position

- All the controls in NORM, AUTO or OFF position

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

12-34-24-869-002

(b) On the center pedestal on the ENG panel 115VU:

1 Put a warning notice to tell persons not to start the engine.

(c) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before

you do this procedure.

(d) On the overhead panel 50VU:

1 Make sure that the ON legend on the ENG/FADEC GND PWR 1(2)

pushbutton switch is off

2 Put a warning notice to tell persons not energize the FADEC 1(2).

(e) Open the Fan Cowl Doors, refer to AMM Task 71-13-00-010-010

(f) Put an access platform in position at the engine.

(g) Deactivate the Thrust Reverse Hydraulic Control Unit, refer to AMM Task

78-30-00-040-012.

(h) Open the Thrust Reverse Halves, refer to AMM Task 78-32-00-010-010.

C. PROCEDURE

(1) Subtask 711064-832-001-001 - Inspect the Serial Number (SN) of the Forward

Engine Mount Crossbeam Attach Pin for Engines 1 and 2 in accordance with VSB

Work Zones and Access Panels

Zone Access/Work location

430

440

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References

Aircraft Maintenance Manual (AMM) Task 71-00-20-000-802

Task 71-00-20-400-802

Vendor Service Bulletin (VSB) UTAS V2500-NAC-71-0323

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do an inspection of the crossbeam attach pin serial numbers for the Engine 1

and/or Engine 2, in accordance with instructions given in UTAS Service Bulletin No.

V2500-NAC-71-0323

NOTE: Make sure the surface to be inspected is clean.

Refer to Fig. A-FFAAA.

1 If the pin serial number is found listed in the VSB:

a Replace the affected attach pin

Refer to Fig. A-FFAAA

<1> Prior to removal and replacement of the affected attach pin, unload

the engine, refer to AMM Task 71-00-20-000-802.

<2> Replace the attach pin in accordance with instructions given in

UTAS Service Bulletin No. V2500-NAC-71-0323.

<3> After replacement of the affected attach pin, reload the engine, refer

to AMM Task 71-00-20-400-802.

b Send the inspection report to Airbus,

Refer to Fig. A-FRAAA

and

No further action.

2 If the pin serial number is not found listed in the VSB, but the aircraft MSN is

found on the list:

a Check the aircraft records for engine removal since aircraft first flight

<1> If the pin serial number does not appear in the effectivity of the

VSB, check the engine maintenance records to verify the current

location of affected pin

and

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SERVICE BULLETIN

Send the inspection report to Airbus, refer to Fig. A-FRAAA.

<2> If engine not removed, contact Airbus and follow their instructions.

<3> If the pin serial number is not found listed in the VSB and neither

the aircraft MSN, no futher actions.

D. TEST

None

E. CLOSE-UP

(1) Subtask 711064-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 71-13-00-410-010

Task 78-30-00-440-012

Task 78-32-00-410-010

(a) Make sure that the work area is clean and clear of tools and other items of

equipment.

(b) Close the Thrust Reverser Halves, refer to AMM Task 78-32-00-410-010.

(c) Activate the Thrust Reverse Hydraulic Control Unit, refer to AMM Task

78-30-00-440-012.

(d) Close the Fan Cowl Doors, refer to AMM Task 71-13-00-410-010.

(e) Remove the access platform(s).

(f) Remove Warning notice(s).

(g) Restore the systems and the aircraft to normal operating conditions.

(h) Put the aircraft back to its initial configuration.

DATE: Nov 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 13

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SERVICE BULLETIN

**CONF ALL

CHECK THE SERIAL NUMBER (SN) OF THE ATTACH PINS FOR 

ENGINE 1 AND / OR ENGINE 2 IN ACCORDANCE WITH

YES LISTED IN THE VSB

PIN SN FOUND

REMOVE AND REPLACE

THE AFFECTED ATTACH PIN ON

SEND THE INSPECTION

REPORT TO AIRBUS

TASK 711064−832−801−001 AT THE THRESHOLD GIVEN

ENGINE 1 AND / OR ENGINE 2

IN ACCORDANCE WITH SUBTASK

QUESTION

ACTION

FINDING

IN THE PLANNING INFORMATION PARAGRAPH E.(2)

711064−832−001−001

NO

SINCE THE AIRCRAFT

ENGINE REPLACED

FIRST FLIGHT

CHECK THE ENGINE

MAINTENANCE RECORDS FOR CURRENT

LOCATION OF AFFECTED ATTACH PIN

CONTACT AIRBUS

AND FOLLOW THEIR

INSTRUCTIONS

YES

SEND THE INSPECTION

REPORT TO AIRBUS

NO

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN

NOTE:

IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE 

AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN 

IN THIS SERVICE BULLETIN N_SB_711064_5_FAAA_01_03

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Nov 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 14

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SERVICE BULLETIN

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−71−1064

DATE OF INSPECTION :

INSPECTION METHOD : DETAILED

INSPECTION

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEEE6

NACELLE SYSTEMS & STRUCTURE

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14

SN OF THE FWD

MOUNT CROSSBEAM

ATTACH PIN LISTED

ON THE VSB

YES NO

ENGINE 1

REPLACED THE FWD

MOUNT CROSSBEAM YES NO

YES NO

YES NO

ENGINE REPLACED

SINCE A/C FIRST

FLIGHT

CHECK MAINT RECORDS

OF REPLACED ENGINE

FOR THE SN OF THE FWD

YES NO

ENGINE 2

YES NO

YES NO

YES NO

REMARKS

ATTACH PIN AS PER VSB

MOUNT CROSSBEAM

ATTACH PIN

N_SB_711064_5_RAAA_01_01

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Nov 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 15

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 16

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SERVICE BULLETIN

Appendix 01: Elapsed Time Assumption

**CONF ALL

For the elapsed time assumption, refer to Fig. A-FAAAA

DATE: Nov 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 1

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SERVICE BULLETIN

Appendix 01: Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−71−1064

JOB SET−UP

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

2.00

1.00

STEPS

1.00 0.50

0

INSPECTION OF THE FORWARD ENGINE

CLOSE−UP 1.00 0.50

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

2

2

:

:

SB ELAPSED TIME

(HOURS)

1

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

MOUNT CROSSBEAM ATTACH PIN REFER TO VENDOR SERVICE BULLETIN

0.5

SERIAL NUMBER FOR ENGINES 1 AND 2

N_SB_711064_5_AAAA_01_01

Figure A-FAAAA - Sheet 01

Appendix 01: Elapsed Time Assumption

DATE: Nov 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: POWER PLANT - GENERAL - FORWARD MOUNT - INSPECTION OF

FORWARD ENGINE MOUNT

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 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 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 05/14 SERVICE BULLETIN No.: A320-71-1064

REVISION No.: 01 - Apr 01/15 Page: 1

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