@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: 57

TITLE: WING - SLAT TRACKS - REPLACE ECCENTRIC BOLTS OF TRACKS 4,

5, 7 AND 8

MODIFICATION No.: 13596B0066

This page transmits Revision No.01 of Service Bulletin No.A310-57-2100

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 separate into two configurations the effectivity of this Service Bulletin, one for

A310-300 aircraft and one for A310-200 aircraft.

- On A310-300 aircraft, the eccentric bolts on slats 2 and 3 at tracks 4, 5, 7 and 8 are replaced

- On A310-200 aircraft, the eccentric bolts on slats 2 at track 5 are replaced

CHANGES

FRONT MATTER

WING - SLAT TRACKS - REPLACE

ECCENTRIC BOLTS OF TRACKS 4, 5, 7

AND 8

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

CONFIGURATION UPDATED

R

MATERIAL PRICE INFORMATION TABLE ADDED N

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MANPOWER ADDED N

Fig. A-USAAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-USAAB FIGURE SOLUTION ADDED N

Fig. A-USAAB Sheet 01 SHEET ADDED N

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition CONFIGURATION LIST UPDATED R

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION ADDED N

Material Effectivity MATERIAL EFFECTIVITY UPDATED

CONFIGURATION UPDATED

MATERIAL SET UPDATED

R

MATERIAL EFFECTIVITY ADDED N

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

Advantages ADVANTAGES UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

R

REFERENCED DOCUMENTATION ADDED N

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED

CONFIGURATION UPDATED

R

PUBLICATIONS AFFECTED ADDED N

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED

CONFIGURATION UPDATED

R

INTERCHANGEABILITY/MIXABILITY ADDED N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL SET UPDATED

MATERIAL AVAILABILITY UPDATED

MATERIAL PRICE UPDATED

R

LIST OF COMPONENTS LIST OF COMPONENTS UPDATED R

Kit 572100B01R01 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

Kit 572100B02R01 PART MATERIAL SET ADDED N

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 2

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@A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

ACCOMPLISHMENT INSTRUCTIONS

TASK 572100- 831-895-001-

MODIFICATION

TASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 572100-910-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 572100-839-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

MANPOWER RESSOURCE UPDATED

R

Subtask 572100-910-401-001 SUBTASK SOLUTION ADDED N

Subtask 572100-839-401-001 SUBTASK SOLUTION ADDED N

Subtask 572100-941-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 572100-941-401-002 SUBTASK SOLUTION ADDED N

Subtask 572100-831-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

PART NUMBER UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PART NUMBER DESCRIPTION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 572100-831-402-001 SUBTASK SOLUTION ADDED N

Subtask 572100-700-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 572100-700-401-002 SUBTASK SOLUTION ADDED N

Subtask 572100-942-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 572100-942-401-002 SUBTASK SOLUTION ADDED N

Fig. A-UBAAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-UBAAA Sheet 01 SHEET UPDATED R

Fig. A-UBAAB FIGURE SOLUTION ADDED N

Fig. A-UBAAB Sheet 01 SHEET ADDED N

FILLING INSTRUCTIONS

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

Replace the complete document.

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jul 29/11

REVISION No. : 01 - Feb 03/12

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 4

7

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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: 57

TITLE: WING - SLAT TRACKS - REPLACE ECCENTRIC BOLTS OF TRACKS 4,

5, 7 AND 8

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13596B0066

MINOR None

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Following a review of eccentric bolt lives and failure conditions, it is now necessary to reclassify bolts as

Principal Structural Elements (PSE’s) and introduce them into the Airworthiness Limitations Section

(ALS) Part 1.

This Service Bulletin (SB) supports the interchangeability of post modification 13596B0066 eccentric

bolts on older aircraft and provides a means of removing the Slat 2 and Slat 3 bolts pn A578-44015-200

and the bolt pn A578-43624-200 and its associated washer pn A578-44016-200 from the fleet. Some

eccentric bolts on Tracks 4, 5, 7 and 8 need to be replaced before reaching their calculated life limit, as

defined below:

- 40,000 Flight Cycles (FC)/66,000 Flight Hours (FH) for average flight time < 4 hours (not applicable

to A310-200 aircraft).

- 31,400 Flight Cycles (FC)/66,000 Flight Hours (FH) for average flight time > 4 hours (not applicable

to A310-200 aircraft).

- 35,900 Flight Cycles (FC)/71,800 Flight Hours (FH) for A310-200 aircraft only.

This Service Bulletin supports the interchangeability of post modification 13596B0066 eccentric bolts

and replaces the affected eccentric bolts:

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 1

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SERVICE BULLETIN

SUMMARY

- on Slats 2 and 3 at tracks 4, 5, 7 and 8 on A310-300 aircraft.

- on Slats 2 at track 5 on A310-200 aircraft.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 572100B01R01 2 50,500.00 Bolt, washer

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 572100B02R01 2 12,960.00 Bolt, washer

EFFECTIVITY

**CONF ALL

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

19U 46T 52X 58X 83V AIC AMV CFC DGA FDX GAF IRA PCA

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 2

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@A310

SERVICE BULLETIN

SUMMARY

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD YES

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 572100-831-895-001: MODIFICATION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 6.00

**CONF 002

Task 572100-831-895-001: MODIFICATION

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.25

APPENDICES

**CONF ALL

None

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 3

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@A310

SERVICE BULLETIN

SUMMARY

**CONF 001

B_SB_572100_7_SAAA_01_00

A B

TRACK 4

TRACK 5

TRACK 7

TRACK 8

SLAT 2

SLAT 3

A

B

Figure A-USAAA - Sheet 01

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 4

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@A310

SERVICE BULLETIN

SUMMARY

**CONF 002

A

TRACK 5

SLAT 2

A

Z521 (Z621)

B_SB_572100_7_SAAB_01_00

Figure A-USAAB - Sheet 01

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 5

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 6

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

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: 57

TITLE: WING - SLAT TRACKS - REPLACE ECCENTRIC BOLTS OF TRACKS 4,

5, 7 AND 8

MODIFICATION No.: 13596B0066

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

310-204 310-222 310-304 310-322 310-324

(2) Effectivity by MSN

0378 0392 0399 0406-0407 0410 0413 0418-0419 0421-0422 0425 0427-0429 0431

0434 0436-0437

(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

46T 0413

52X 0410

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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@A310

SERVICE BULLETIN

OPERATOR MSN

58X 0431

83V 0427

AIC 0392 0406 0407 0428 0429

AMV 0437

CFC 0425

DGA 0418 0421 0422

FDX 0378

GAF 0434

IRA 0436

PCA 0419

(4) Configuration by MSN

MSN CONFIGURATION

0378 0392 0399 0406 0407 0410 0413 0418 0421 0422 0425

0428 0429 0431 0434 0436 0437

001

0419 0427 002

(5) Configuration definition

**CONF 001

Config. 001 is valid for all A310-300 aircraft given in the effectivity of this Service

Bulletin.

**CONF 002

Config. 002 is valid for all A310-200 aircraft given in the effectivity of this Service

Bulletin.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 572100B01R01 2

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 572100B02R01 2

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 2

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@A310

SERVICE BULLETIN

C. REASON

(1) History

Following a review of eccentric bolt lives and failure conditions, it is now necessary to

reclassify bolts as Principal Structural Elements (PSE’s) and introduce them into the

Airworthiness Limitations Section (ALS) Part 1.

(2) Objective/Action

This Service Bulletin (SB) supports the interchangeability of post modification

13596B0066 eccentric bolts on older aircraft and provides a means of removing the

Slat 2 and Slat 3 bolts pn A578-44015-200 and the bolt pn A578-43624-200 and its

associated washer pn A578-44016-200 from the fleet. Some eccentric bolts on Tracks 4,

5, 7 and 8 need to be replaced before reaching their calculated life limit, as defined

below:

- 40,000 Flight Cycles (FC)/66,000 Flight Hours (FH) for average flight time < 4 hours

(not applicable to A310-200 aircraft).

- 31,400 Flight Cycles (FC)/66,000 Flight Hours (FH) for average flight time > 4 hours

(not applicable to A310-200 aircraft).

- 35,900 Flight Cycles (FC)/71,800 Flight Hours (FH) for A310-200 aircraft only.

(3) Advantages

This Service Bulletin supports the interchangeability of post modification 13596B0066

eccentric bolts and replaces the affected eccentric bolts:

- on Slats 2 and 3 at tracks 4, 5, 7 and 8 on A310-300 aircraft.

- on Slats 2 at track 5 on A310-200 aircraft.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 572100-831-895-001: MODIFICATION

(1) MODIFICATION OF ECCENTRIC BOLT ON SLATS 2 AND 3 ON TRACKS 4, 5, 7

AND 8

**CONF 002

Task 572100-831-895-001: MODIFICATION

(1) MODIFICATION OF ECCENTRIC BOLT ON SLATS 2 ON TRACK 5

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 3

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@A310

SERVICE BULLETIN

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

40,000 Flight Cycles (FC) / 66,000 Flight Hours (FH) for average flight time < 4 hours

(not applicable to A310-200 aircraft).

31,400 Flight Cycles (FC) / 66,000 Flight Hours (FH) for average flight time > 4 hours

(not applicable to A310-200 aircraft).

35,900 Flight Cycles (FC) / 71,800 Flight Hours (FH) for A310-200 aircraft only.

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

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

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

and/or intervals and/or date) given above but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

F. APPROVAL

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

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 572100-831-895-001: MODIFICATION

Get Access 1.00

On Aircraft

MODIFICATION OF ECCENTRIC BOLT ON SLATS 2

AND 3 ON TRACKS 4, 5, 7 AND 8

6.00

Tests 1.00

Close-Up 1.00

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 4

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SERVICE BULLETIN

Task 572100-831-895-001: MODIFICATION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 6.00

**CONF 002

Task 572100-831-895-001: MODIFICATION

Get Access 0.50

On Aircraft

MODIFICATION OF ECCENTRIC BOLT ON SLATS 2

ON TRACK 5

1.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.25

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 20-21-12 27-80-14

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-40-21 51-40-44 51-76-10

**CONF 002

Aircraft Maintenance Manual (AMM) 20-21-12 27-80-14

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-40-21 51-40-44 51-76-10

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

**CONF ALL

K. PUBLICATION AFFECTED

**CONF 001

Airworthiness Limitation Section (ALS) Airworthiness Limitation Section

(ALS) Part 1

Illustrated Parts Catalog (IPC) 57-43-11 57-44-11

**CONF 002

Airworthiness Limitation Section (ALS) Airworthiness Limitation Section

(ALS) Part 1

Illustrated Parts Catalog (IPC) 57-43-11

**CONF ALL

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bolt A5784401520000 A5784401520400 03 Not

Applicable

(1)

Bolt A5784362420000 A5784362420200 03 Not

Applicable

(1)

Washer A5784401620000 A5784439120000 03 Not

Applicable

(1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable between slats or between aircraft but is interchangeable

between tracks on same slat.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bolt A5784362420000 A5784362420200 03 Not

Applicable

(1)

Washer A5784401620000 A5784439120000 03 Not

Applicable

(1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable between slats or between aircraft but is interchangeable

between tracks on same slat.

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 6

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SERVICE BULLETIN

**CONF ALL

M. SPARES

None

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 7

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 572100B01R01

Kit 572100B02R01

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

For ordering of single spares by fax: +49 40

50 76 40 13

(2) Price and Availability

Kit 572100B01R01

Cost 25,250.00 USD

Availability 90 calendar days from receipt of order

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

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

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

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

at the issue date of the Service Bulletin.

Kit 572100B02R01

Cost 6,480.00 USD

Availability 90 calendar days from receipt of order

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

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

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

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 9

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@A310

SERVICE BULLETIN

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

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

As a special policy applied to this Service Bulletin, AIRBUS will provide a 10% reduction to

the applicable sales prices given in the paragraph ’Price and Availability’ for orders placed

before 31-Dec-2018.

C. LIST OF COMPONENTS

Kit 572100B01R01

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

NOTES

1 MS24665-374 4 Pin

3 A5784439120000 1 Washer (3) A5784401620000 03

5 A5784401520400 3 Bolt (5) A5784401520000 03

8 A5784362420200 1 Bolt (8) A5784362420000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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.

Kit 572100B02R01

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

NOTES

1 MS24665-374 1 Pin

3 A5784439120000 1 Washer (3) A5784401620000 03

8 A5784362420200 1 Bolt (8) A5784362420000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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

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

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

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

F. TOOLING

None

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 12

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 572100-831-895-001 - MODIFICATION

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, CLEANING.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 6.00

**CONF 002

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.25

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 572100-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 20-21-12, Page Block 001

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-40-21

51-40-44

51-76-10

(a) For information on tightening torques for standard threaded fasteners, refer to AMM

20-21-12, Page Block 001.

(b) For fastener installation and removal, refer to SRM 51-40-21.

(c) For fastener hole and drill data, refer to SRM 51-40-44.

(d) For repair of sealing and sealing of fasteners, refer to SRM 51-76-10.

(2) Subtask 572100-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 572100-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 20-21-12, Page Block 001

Structural Repair Manual (SRM) 51-40-21

51-40-44

51-76-10

(a) For information on tightening torques for standard threaded fasteners, refer to AMM

20-21-12, Page Block 001.

(b) For fastener installation and removal, refer to SRM 51-40-21.

(c) For fastener hole and drill data, refer to SRM 51-40-44.

(d) For repair of sealing and sealing of fasteners, refer to SRM 51-76-10.

(2) Subtask 572100-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 572100-941-401-001 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

(a) Do the Job Set-Up procedure for the ’Removal of the tracks on slats 2 and 3’

(Refer to AMM 27-80-14, Page Block 401).

**CONF 002

(1) Subtask 572100-941-401-002 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

(a) Do the Job Set-Up procedure for the ’Removal of the tracks on slat 2’ (Refer to

AMM 27-80-14, Page Block 401).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 572100-831-401-001 - MODIFICATION OF ECCENTRIC BOLT ON SLATS 2

AND 3 ON TRACKS 4, 5, 7 AND 8

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

Material necessary to do the job

Kit 572100B01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS24665-374 4 Pin

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 A5784439120000 1 Washer

5 A5784401520400 3 Bolt

8 A5784362420200 1 Bolt

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

Fig. A-UBAAA

Eccentric Bolt Replacement (Tracks 4, 5,

7 and 8)

Sheet 01

NOTE: The worksteps that follow are applicable to both the Left Hand and Right

Hand Wings.

(a) Remove and replace each of the eccentric bolts at slat tracks 4, 7 and 8 one at a

time (Refer to AMM 27-80-14, Page Block 401).

Refer to Fig. A-UBAAA Sheet 01

NOTE: Only remove one eccentric bolt at a time.

NOTE: Only instructions to replace the eccentric bolts are shown, for a

detailed description of all parts, materials and detailed instructions

refer to AMM 27-80-14, Page Block 401.

1 Mark and record each eccentric bolts red line before removal; so it can be

reinstalled (or replace by a new bolt) in the same position.

2 Remove

6 Nut Item (4) Retain

6 Bolt Item (7) Retain

6 Lockplate Item (6) Retain

3 Remove

3 Cotter pin Item (1) Discard

3 Nut Item (2) Retain

3 Washer Item (3) Retain

3 Bolt A5784401520000 Item (5) Discard

4 Install new

3 Bolt A5784401520400 Item 5

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SERVICE BULLETIN

5 Reinstall

3 Washer Item (3) Retained at

removal

3 Nut Item (2) Retained at

removal

6 Install new

3 Cotter Pin MS24665-374 Item 1

7 Reinstall the

6 Lockplate Item (6) Retained at

removal

NOTE: The lockplates can be reversed to provide a half serration

adjustment on installation.

8 Reinstall the

6 Nut Item (4) Retained at

removal

6 Bolt Item (7) Retained at

removal

(b) Replace the eccentric bolt at slat track 5 (Refer to AMM 27-80-14, Page Block

401).

Refer to Fig. A-UBAAA Sheet 01

NOTE: Only instructions to replace the eccentric bolts are shown, for a

detailed description of all parts, materials and detailed instructions

refer to AMM 27-80-14, Page Block 401.

1 Remove

2 Nut Item (4) Retain

2 Bolt Item (7) Retain

2 Lockplate Item (6) Retain

2 Remove

1 Cotter pin Item (1) Discard

1 Nut Item (2) Retain

1 Bolt A5784362420000 Item (8) Discard

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

1 Washer A5784401620000 Item (3) Discard

3 Install new

1 Bolt A5784362420200 Item 8

1 Washer A5784439120000 Item 3

4 Reinstall the

1 Nut Item (2) Retained at

removal

5 Install new

1 Cotter Pin MS24665-374 Item 1

6 Reinstall the

2 Lockplate Item (6) Retained at

removal

NOTE: The lockplates can be reversed to provide a half serration

adjustment on installation.

7 Reinstall the

2 Nut Item (4) Retained at

removal

2 Bolt Item (7) Retained at

removal

**CONF 002

(1) Subtask 572100-831-402-001 - MODIFICATION OF ECCENTRIC BOLT ON SLATS 2

ON TRACK 5

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Kit 572100B02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS24665-374 1 Pin

3 A5784439120000 1 Washer

8 A5784362420200 1 Bolt

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

Fig. A-UBAAB

Eccentric Bolt Replacement (Track 5

only)

Sheet 01

NOTE: The worksteps that follow are applicable to both the Left Hand and Right

Hand Wings.

(a) Replace the eccentric bolt at slat track 5 (Refer to AMM 27-80-14, Page Block

401).

Refer to Fig. A-UBAAB Sheet 01

NOTE: Only instructions to replace the eccentric bolts are shown, for a

detailed description of all parts, materials and detailed instructions

refer to AMM 27-80-14, Page Block 401.

1 Remove

2 Nut Item (4) Retain

2 Bolt Item (7) Retain

2 Lockplate Item (6) Retain

2 Remove

1 Cotter pin Item (1) Discard

1 Nut Item (2) Retain

1 Bolt A5784362420000 Item (8) Discard

1 Washer A5784401620000 Item (3) Discard

3 Install new

1 Bolt A5784362420200 Item 8

1 Washer A5784439120000 Item 3

4 Reinstall the

1 Nut Item (2) Retained at

removal

5 Install new

1 Cotter Pin MS24665-374 Item 1

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

6 Reinstall the

2 Lockplate Item (6) Retained at

removal

NOTE: The lockplates can be reversed to provide a half serration

adjustment on installation.

7 Reinstall the

2 Nut Item (4) Retained at

removal

2 Bolt Item (7) Retained at

removal

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 572100-700-401-001 - TEST

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

(a) Do the tests specified in the procedure for the ’Installation of the tracks on slats 2

and 3’ (Refer to AMM 27-80-14, Page Block 401).

**CONF 002

(1) Subtask 572100-700-401-002 - TEST

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

(a) Do the tests specified in the procedure for the ’Installation of the tracks on slat 2’

(Refer to AMM 27-80-14, Page Block 401).

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 572100-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

(a) Do the Close-Up procedure for the ’Installation of the tracks on slats 2 and 3’

(Refer to AMM 27-80-14, Page Block 401).

**CONF 002

(1) Subtask 572100-942-401-002 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 27-80-14, Page Block 401

(a) Do the Close-Up procedure for the ’Installation of the tracks on slat 2’ (Refer to

AMM 27-80-14, Page Block 401).

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

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SERVICE BULLETIN

**CONF 001

A B

TRACK 4

TRACK 5

TRACK 7

TRACK 8

SLAT 2

C SLAT 3

D

E

F

LINK

KNUCKLE

A

B

C E F

Z522 (Z622)

KNUCKLE

D

Z521 (Z621)

LINK

B_SB_572100_7_BAAA_01_03

Figure A-UBAAA - Sheet 01

Eccentric Bolt Replacement (Tracks 4, 5, 7 and 8)

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 22

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SERVICE BULLETIN

**CONF 002

A

TRACK 5

SLAT 2

LINK

KNUCKLE

A

Z521 (Z621)

B

B

B_SB_572100_7_BAAB_01_02

Figure A-UBAAB - Sheet 01

Eccentric Bolt Replacement (Track 5 only)

DATE: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 23

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SERVICE BULLETIN

REPORTING SHEET

TITLE: WING - SLAT TRACKS - REPLACE ECCENTRIC BOLTS OF TRACKS 4,

5, 7 AND 8

MODIFICATION No.: 13596B0066

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: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 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: Jul 29/11 SERVICE BULLETIN No.: A310-57-2100

REVISION No.: 01 - Feb 03/12 Page: 1

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