@A300-600

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 57

TITLE: WINGS-STRUCTURE-INSPECTION OF FR40 LOWER JUNCTION

FASTENER HOLES

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Following A300-600 Extended Service Goal 2 (ESG2) study, some specific inspections for cracks have

been performed in fittings of frame 40 (FR40) at areas not covered by any existing tasks. Some findings

were then identified on retired A300-600 aircraft in lower tension bolt area rib one junction (both sides).

After laboratory analysis, it has been decided to launch inspection of all concerned in-service aircraft.

This Service Bulletin mandates a repetitive High Frequency Eddy Current (HFEC) inspection on fitting

around fastener heads located FR40 - lower wing junction or a Rototest inspection of all concerned inservice aircraft.

Accomplishment of this Service Bulletin will contribute to prevent fitting cracking, which may lead to

complex repair.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 1

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@A300-600

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 2 See SB Bolts, Nuts

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA02 2 See SB Bolts, Nuts

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA03 2 See SB Bolts, Nuts

EFFECTIVITY

**CONF ALL

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

67Q ABD ABR AHK BCS CES F2I FDX GBG I2L IRA IRM KAC

MGC MNB MON MRJ MSR MXU SUD TAR THA TMA UPS URS UZB

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 2

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

SERVICE BULLETIN

SUMMARY

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

TOTAL MANHOURS 11.50

ELAPSED TIME (HOURS) 5.75

**CONF 002

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

TOTAL MANHOURS 43.00

ELAPSED TIME (HOURS) 21.50

**CONF 003

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

TOTAL MANHOURS 43.00

ELAPSED TIME (HOURS) 21.50

APPENDICES

**CONF ALL

Appendix 01: Elapsed Time Assumption

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 3

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@A300-600

SERVICE BULLETIN

SUMMARY

**CONF ALL

INSPECTION AREA

NOTE:

B

FR40

RH SHOWN

LH SYMMETRICAL

A

B

A Z140

B

D_SB_576115_5_SAAA_01_02

Figure A-FSAAA - Sheet 01

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 4

5

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

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 57

TITLE: WINGS-STRUCTURE-INSPECTION OF FR40 LOWER JUNCTION

FASTENER HOLES

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620 F4-605R

F4-622R

(2) Effectivity by MSN

0294 0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479

0505 0521 0525 0529-0530 0532 0536 0543 0546 0553 0555 0557-0559 0561 0563

0572 0575 0577 0579 0581 0584 0602-0605 0607-0608 0611 0613 0617-0618 0621

0623 0625-0626 0629-0630 0632-0633 0637 0641 0643 0657 0659 0664 0666 0668

0670 0673 0677 0679 0681 0683 0688 0694 0696 0699 0701 0703 0705 0707 0709

0711 0713 0715 0717 0719 0721-0730 0732-0746 0748-0750 0752-0764 0766-0775

0777-0794 0797 0799-0840 0845-0878

(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.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 1

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@A300-600

SERVICE BULLETIN

OPERATOR MSN

67Q 0584 0603 0744 0749 0764

ABD 0557

ABR 0683 0770

AHK 0855 0856 0857 0858 0859 0860 0870 0871

BCS 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730

0737 0740 0753 0783 0797 0836 0837

CES 0707 0725 0732 0741 0746 0754 0763

F2I 0294 0529

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

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

0668 0688 0709 0713 0715 0726 0728 0735 0736 0738 0742 0745

0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774

0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799

0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878

GBG 0626 0643

I2L 0677

IRA 0632 0696 0723 0727

IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701

0773 0838

KAC 0344 0673 0694 0699 0719 0721

MGC 0743

MNB 0521 0525 0532 0734 0739 0755 0756 0758

MON 0604 0605

MRJ 0750 0762

MSR 0561 0607

MXU 0767 0788

SUD 0666 0775

TAR 0505 0558 0563

THA 0577 0629 0681 0705 0782 0784 0785 0786 0787

TMA 0872

UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816

0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828

0829 0830 0831 0832 0833 0834 0835 0839 0840 0845 0846 0847

0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865

0866 0867 0868 0869

URS 0733

UZB 0717 0722

(4) Configuration by MSN

MSN CONFIGURATION

0294 0344 0358 0361 0380 0401 0405 0408 0411 0414 0505

0546 0553 0558 0563 0584 0602 0608 0617 0618 0621 0623

0626 0632 0637 0641 0643 0670 0679 0683 0694 0696 0699

0701 0703 0711 0719 0721 0723 0724

001 003

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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@A300-600

SERVICE BULLETIN

MSN CONFIGURATION

0365 0388 0417 0477 0479 0521 0525 0529 0530 0532 0536

0543 0555 0557 0559 0561 0572 0575 0577 0579 0581 0603

0604 0605 0607 0611 0613 0625 0629 0630 0633 0657 0659

0664 0666 0668 0673 0677 0681 0688 0705 0707 0709 0713

0715 0717 0722 0725

003

0726 0727 0728 0729 0730 0732 0733 0734 0735 0736 0737

0738 0739 0740 0741 0742 0743 0744 0745 0746 0748 0749

0750 0752 0753 0754 0755 0756 0757 0758 0759 0760 0761

0762 0763 0764 0766 0767 0768 0769 0770 0771 0772 0773

0774 0775 0777 0778 0779 0780 0781 0782 0783 0784 0785

0786 0787 0788 0789 0790 0791 0792 0793 0794 0797 0799

0800 0801 0802 0803 0804 0805 0806 0807 0808 0809 0810

0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821

0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832

0833 0834 0835 0836 0837 0838 0839 0840 0845 0846 0847

0848 0849 0850 0851 0852 0853 0854 0855 0856 0857 0858

0859 0860 0861 0862 0863 0864 0865 0866 0867 0868 0869

0870 0871 0872 0873 0874 0875 0876 0877 0878

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Mod. No. 10221S20394 is not embodied and

SB No. A300-57-6053 is not accomplished.

**CONF 002

Config. 002 is valid for aircraft on which Mod. No. 10221S20394 is embodied and SB

No. A300-57-6053 is not accomplished.

**CONF 003

Config. 003 is valid for aircraft on which Mod. No. 10221S20394 is not embodied ans SB

No. A300-57-6053 is accomplished.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 2

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Component COMPA02 2

Consumable CMLA01 1

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 3

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@A300-600

SERVICE BULLETIN

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Component COMPA03 2

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Following A300-600 Extended Service Goal 2 (ESG2) study, some specific inspections

for cracks have been performed in fittings of frame 40 (FR40) at areas not covered by

any existing tasks. Some findings were then identified on retired A300-600 aircraft in

lower tension bolt area rib one junction (both sides). After laboratory analysis, it has

been decided to launch inspection of all concerned in-service aircraft.

(2) Objective/Action

This Service Bulletin mandates a repetitive High Frequency Eddy Current (HFEC)

inspection on fitting around fastener heads located FR40 - lower wing junction or a

Rototest inspection of all concerned in-service aircraft.

(3) Advantages

Accomplishment of this Service Bulletin will contribute to prevent fitting cracking, which

may lead to complex repair.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

NOTE: To accomplish this Service Bulletin, two possibilities are available:

- Either do an HFEC Inspection as described in TASK 576115-832-801 001

Do an HFEC Inspection of FR40 Lower Wing Junction Fastener Holes

- Or do a Rototest Inspection as described in TASK 576115-832-803 001

Do a Rototest Inspection of FR40 Lower Wing Junction Fastener Holes

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 4

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@A300-600

SERVICE BULLETIN

Holes

(1) Do an HFEC Inspection around fasteners at LH Side

(2) Do an HFEC Inspection around fasteners at RH Side

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

(1) Remove the Fasteners from LH Side

(2) Remove the Fasteners from RH Side

(3) Do a Rototest Inspection of Fasteners Holes at LH Side

(4) Do a Rototest Inspection of Fasteners Holes at RH Side

(5) Install New Fasteners on LH Side

(6) Install New Fasteners on RH Side

**CONF 002

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

(1) Do an HFEC Inspection around fasteners at LH Side

(2) Do an HFEC Inspection around fasteners at RH Side

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

(1) Remove the Fasteners from LH Side

(2) Remove the Fasteners from RH Side

(3) Do a Rototest Inspection of Fasteners Holes at LH Side

(4) Do a Rototest Inspection of Fasteners Holes at RH Side

(5) Install New Fasteners on LH Side

(6) Install New Fasteners on RH Side

**CONF 003

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

(1) Do an HFEC Inspection around fasteners at LH Side

(2) Do an HFEC Inspection around fasteners at RH Side

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 5

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@A300-600

SERVICE BULLETIN

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

(1) Remove the Fasteners from LH Side

(2) Remove the Fasteners from RH Side

(3) Do a Rototest Inspection of Fasteners Holes at LH Side

(4) Do a Rototest Inspection of Fasteners Holes at RH Side

(5) Install New Fasteners on LH Side

(6) Install New Fasteners on RH Side

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

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

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

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

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

mandated accomplishment timescale.

Table 1, Config. 001 - Do an HFEC Inspection of FR40 Lower Wing Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

All aircraft on which the

rototest inspection has

not been done.

Do an HFEC inspection

on fitting around FR40

lower wing junction

fastener heads, refer to

subtask

576115-832-002-001 for

RH side and subtask

576115-832-009-001 for

LH side (TASK

576115-832-801-001).

Within 1000 FH from

Service Bulletin issue

date.

None

No cracks found Repeat the inspection,

refer to TASK

576115-832-801-001.

None Every 1000 FH until

Rototest Inspection is

done

See NOTE (*)

Cracks found Contact Airbus Before next flight None

NOTE (*): Repetitive HFEC inspection is no more required if rototest inspection is done within 1000

FH from Service Bulletin issue date.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 6

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@A300-600

SERVICE BULLETIN

Table 2, Config. 001 - Do a Detailed (DET) Inspection and a rototest inspection of FR40 Lower Wing

Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

All aircraft Remove the FR40 lower

junction fastener and

measure the diameter of

the holes, refer to

subtask

576115-000-003-001 for

RH side and

576115-000-004-001 for

LH side (TASK

576115-832-803-001)

Before 36 months from

Service Bulletin issue

date.

None

Diameter of the holes

are not in tolerance of

Fig. A-FBBAA Sheet 03

Table 1 (nominal

diameter) and are not in

tolerance of Fig. AFBBAA Sheet 03 Table

2 (first and second

oversize)

Contact Airbus Before next flight None

Diameter of the holes

are in tolerance of Fig.

A-FBBAA Sheet 03

Table 1 (nominal

diameter)

Do a detailed (DET)

inspection and a rototest

inspection of the

fastener holes, refer to

substask

576115-832-007-001 for

RH side and subtask

576115-832-008-001 for

LH side (TASK

576115-832-803-001)

Before next flight None

Cracks found Contact Airbus Before next flight None

Install new fasteners,

refer to subtask

576115-400-003-001 for

RH side and subtask

576115-400-004-001 for

LH side (TASK

576115-832-803-001)

And

No cracks found Before next flight None

Repeat the inspection,

refer to TASK

576115-832-803-001

None Every 7000 FC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 7

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@A300-600

SERVICE BULLETIN

Table 2, Config. 001 - Do a Detailed (DET) Inspection and a rototest inspection of FR40 Lower Wing

Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

Diameter of the holes

are not in tolerance of

Fig. A-FBBAA Sheet 03

Table 1 (nominal

diameter) but are in

tolerance of Fig. AFBBAA Sheet 03 Table

2 (first and second

oversize)

Do a detailed (DET)

inspection and a rototest

inspection of the

fastener holes, refer to

substask

576115-832-007-001 for

RH side and subtask

576115-832-008-001 for

LH side (TASK

576115-832-803-001)

Before next flight None

Cracks found Contact Airbus Before next flight None

Install new fasteners,

refer to subtask

576115-400-003-001 for

RH side and subtask

576115-400-004-001 for

LH side (TASK

576115-832-803-001)

And

No cracks found Before next flight None

Repeat the inspection,

refer to TASK

576115-832-803-001

None Every 7000 FC

**CONF 002

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

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

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

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

mandated accomplishment timescale.

Table 1, Config. 002 - Do an HFEC Inspection of FR40 Lower Wing Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

All aircraft on which the

rototest inspection has

not been done.

Do an HFEC inspection

on fitting around FR40

lower wing junction

fastener heads, refer to

subtask

576115-832-002-001 for

RH side and subtask

576115-832-009-001 for

LH side (TASK

576115-832-801-001).

Within 1000 FH from

Service Bulletin issue

date.

None

No cracks found Repeat the inspection,

refer to TASK

576115-832-801-001.

None Every 1000 FH until

Rototest Inspection is

done

See NOTE (*)

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 8

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@A300-600

SERVICE BULLETIN

Table 1, Config. 002 - Do an HFEC Inspection of FR40 Lower Wing Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

Cracks found Contact Airbus Before next flight None

NOTE (*): Repetitive HFEC inspection is no more required if rototest inspection is done within 1000

FH from Service Bulletin issue date.

Table 2, Config. 002 - Do a Detailed (DET) Inspection and a rototest inspection of FR40 Lower Wing

Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

All aircraft Remove the FR40 lower

junction fastener and

measure the diameter of

the holes, refer to

subtask

576115-000-003-002 for

RH side and

576115-000-004-002 for

LH side (TASK

576115-832-803-001)

Before 36 months from

Service Bulletin issue

date.

None

Diameter of the holes

are not in tolerance of

Fig. A-FBBAA Sheet 03

Table 1 (nominal

diameter) and are not in

tolerance of Fig. AFBBAA Sheet 03 Table

2 (first and second

oversize)

Contact Airbus Before next flight None

Diameter of the holes

are in tolerance of Fig.

A-FBBAA Sheet 03

Table 1 (nominal

diameter)

Do a detailed (DET)

inspection and a rototest

inspection of the

fastener holes, refer to

substask

576115-832-007-001 for

RH side and subtask

576115-832-008-001 for

LH side (TASK

576115-832-803-001)

Before next flight None

Cracks found Contact Airbus Before next flight None

Install new fasteners,

refer to subtask

576115-400-003-002 for

RH side and subtask

576115-400-004-002 for

LH side (TASK

576115-832-803-001)

And

No cracks found Before next flight None

Repeat the inspection,

refer to TASK

576115-832-803-001

None Every 7000 FC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 9

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SERVICE BULLETIN

Table 2, Config. 002 - Do a Detailed (DET) Inspection and a rototest inspection of FR40 Lower Wing

Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

Diameter of the holes

are not in tolerance of

Fig. A-FBBAA Sheet 03

Table 1 (nominal

diameter) but are in

tolerance of Fig. AFBBAA Sheet 03 Table

2 (first and second

oversize)

Do a detailed (DET)

inspection and a rototest

inspection of the

fastener holes, refer to

substask

576115-832-007-001 for

RH side and subtask

576115-832-008-001 for

LH side (TASK

576115-832-803-001)

Before next flight None

Cracks found Contact Airbus Before next flight None

Install new fasteners,

refer to subtask

576115-400-003-002 for

RH side and subtask

576115-400-004-002 for

LH side (TASK

576115-832-803-001)

And

No cracks found Before next flight None

Repeat the inspection,

refer to TASK

576115-832-803-001

None Every 7000 FC

**CONF 003

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

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

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

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

mandated accomplishment timescale.

Table 1, Config. 003 - Do an HFEC Inspection of FR40 Lower Wing Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

All aircraft on which the

rototest inspection has

not been done.

Do an HFEC inspection

on fitting around FR40

lower wing junction

fastener heads, refer to

subtask

576115-832-002-001 for

RH side and subtask

576115-832-009-001 for

LH side (TASK

576115-832-801-001).

Within 1000 FH from

Service Bulletin issue

date.

None

No cracks found Repeat the inspection,

refer to TASK

576115-832-801-001.

None Every 1000 FH until

Rototest Inspection is

done

See NOTE (*)

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 10

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SERVICE BULLETIN

Table 1, Config. 003 - Do an HFEC Inspection of FR40 Lower Wing Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

Cracks found Contact Airbus Before next flight None

NOTE (*): Repetitive HFEC inspection is no more required if rototest inspection is done within 1000

FH from Service Bulletin issue date.

Table 2, Config. 003 - Do a Detailed (DET) Inspection and a rototest inspection of FR40 Lower Wing

Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

All aircraft Remove the FR40 lower

junction fastener and

measure the diameter of

the holes, refer to

subtask

576115-000-003-003 for

RH side and

576115-000-004-003 for

LH side (TASK

576115-832-803-001)

Before 36 months from

Service Bulletin issue

date.

None

Diameter of the holes

are not in tolerance of

Fig. A-FBBAA Sheet 03

Table 1 (nominal

diameter) and are not in

tolerance of Fig. AFBBAA Sheet 03 Table

2 (first and second

oversize)

Contact Airbus Before next flight None

Diameter of the holes

are in tolerance of Fig.

A-FBBAA Sheet 03

Table 1 (nominal

diameter)

Do a detailed (DET)

inspection and a rototest

inspection of the

fastener holes, refer to

substask

576115-832-007-001 for

RH side and subtask

576115-832-008-001 for

LH side (TASK

576115-832-803-001)

Before next flight None

Cracks found Contact Airbus Before next flight None

Install new fasteners,

refer to subtask

576115-400-003-003 for

RH side and subtask

576115-400-004-003 for

LH side (TASK

576115-832-803-001)

And

No cracks found Before next flight None

Repeat the inspection,

refer to TASK

576115-832-803-001

None Every 7000 FC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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Table 2, Config. 003 - Do a Detailed (DET) Inspection and a rototest inspection of FR40 Lower Wing

Junction Fastener Holes

Condition Action Compliance Time Repetitive Interval

Diameter of the holes

are not in tolerance of

Fig. A-FBBAA Sheet 03

Table 1 (nominal

diameter) but are in

tolerance of Fig. AFBBAA Sheet 03 Table

2 (first and second

oversize)

Do a detailed (DET)

inspection and a rototest

inspection of the

fastener holes, refer to

substask

576115-832-007-001 for

RH side and subtask

576115-832-008-001 for

LH side (TASK

576115-832-803-001)

Before next flight None

Cracks found Contact Airbus Before next flight None

Install new fasteners,

refer to subtask

576115-400-003-003 for

RH side and subtask

576115-400-004-003 for

LH side (TASK

576115-832-803-001)

And

No cracks found Before next flight None

Repeat the inspection,

refer to TASK

576115-832-803-001

None Every 7000 FC

**CONF ALL

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

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

included.

For an explanation of the manhours and elapsed time, refer to the Gantt Charts given in

Appendix 01: Elapsed Time Assumption .

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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**CONF 001

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

Get Access 2.00

On Aircraft

Do an HFEC Inspection around fasteners at LH Side 1.50

Do an HFEC Inspection around fasteners at RH Side 1.50

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

Get Access 2.00

On Aircraft

Remove the Fasteners from LH Side 1.00

Remove the Fasteners from RH Side 1.00

Do a Rototest Inspection of Fasteners Holes at LH

Side

1.50

Do a Rototest Inspection of Fasteners Holes at RH

Side

1.50

Install New Fasteners on LH Side 1.00

Install New Fasteners on RH Side 1.00

Close-Up 2.50

TOTAL MANHOURS 11.50

ELAPSED TIME (HOURS) 5.75

**CONF 002

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

Get Access 2.00

On Aircraft

Do an HFEC Inspection around fasteners at LH Side 1.50

Do an HFEC Inspection around fasteners at RH Side 1.50

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

Get Access 12.00

On Aircraft

Remove the Fasteners from LH Side 1.00

Remove the Fasteners from RH Side 1.00

Do a Rototest Inspection of Fasteners Holes at LH

Side

1.50

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 13

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SERVICE BULLETIN

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

Do a Rototest Inspection of Fasteners Holes at RH

Side

1.50

Install New Fasteners on LH Side 1.00

Install New Fasteners on RH Side 1.00

Close-Up 24.00

TOTAL MANHOURS 43.00

ELAPSED TIME (HOURS) 21.50

**CONF 003

Task 576115-832-801-001: Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

Get Access 2.00

On Aircraft

Do an HFEC Inspection around fasteners at LH Side 1.50

Do an HFEC Inspection around fasteners at RH Side 1.50

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

Task 576115-832-803-001: Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

Get Access 12.00

On Aircraft

Remove the Fasteners from LH Side 1.00

Remove the Fasteners from RH Side 1.00

Do a Rototest Inspection of Fasteners Holes at LH

Side

1.50

Do a Rototest Inspection of Fasteners Holes at RH

Side

1.50

Install New Fasteners on LH Side 1.00

Install New Fasteners on RH Side 1.00

Close-Up 24.00

TOTAL MANHOURS 43.00

ELAPSED TIME (HOURS) 21.50

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

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J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 06-41-00

06-41-57 24-00-00 32-12-11

36-11-00 57-41-41

Consumable Material List (CML)

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

Non Destructive Test Manual (NTM) 51-10-01 51-10-08

Standards Manual (SM)

Structural Repair Manual (SRM) 51-24-00 51-40-00 51-40-12

51-40-13 51-40-20 51-40-30

**CONF 002

Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 06-41-00

06-41-57 24-00-00 28-00-00

28-10-00 28-11-00 28-11-29

28-25-00 32-12-11 36-11-00

57-41-41

Consumable Material List (CML)

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

Non Destructive Test Manual (NTM) 51-10-01 51-10-08

Standards Manual (SM)

Structural Repair Manual (SRM) 51-24-00 51-40-00 51-40-12

51-40-13 51-40-20 51-40-30

**CONF 003

Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 06-41-00

06-41-57 24-00-00 28-00-00

28-10-00 28-11-00 28-11-29

28-25-00 32-12-11 36-11-00

57-41-41

Consumable Material List (CML)

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

Non Destructive Test Manual (NTM) 51-10-01 51-10-08

Standards Manual (SM)

Structural Repair Manual (SRM) 51-24-00 51-40-00 51-40-12

51-40-13 51-40-20 51-40-30

**CONF ALL

K. PUBLICATION AFFECTED

Impact on Scheduled Maintenance: refer to Maintenance Planning Document (MPD)

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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M. SPARES

None

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive

multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers

with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to

B/E Aerospace. The address is:

Component COMPA01

Component COMPA02

Component COMPA03

B/E AEROSPACE INC.

CONSUMABLES MANAGEMENT

10000 NW 15th Terrace Miami

FL 33172

USA

Tel EMEA: +49 (0) 40 822 285 31500

Tel US: +1 305 925 2600

Tel ASIA: +1 310 900 1300

Fax EMEA: +49 (0) 40 822 285 31010

Fax US: +1 305 507 7191

Fax ASIA: +1 310 819 1200

SITA: MIAMMCR

E-Mail: AOGdesk_CMG@beaerospace.com

Internet: http://www.beconsumables.com

or, alternatively any other source on the open

market.

(2) Price and Availability

No AIRBUS kit will be provided.

Operator supplied standard hardware parts required to accomplish this Service Bulletin

are to be supplied from the operator’s stock.

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

No Kit

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

Polysulfide Sealant - Fuel Tank

Brushable

06ABA1 As required

Non Aqueous Cleaner - General 08BAA9 As required

(2) Components

Component COMPA01

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

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

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: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Component COMPA02

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

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

5 EN6114V5-15 1 BOLT

6 ASNA2529-5 1 NUT

7 EN6114V6-15 1 BOLT

8 ASNA2529-6 1 NUT

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.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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SERVICE BULLETIN

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Component COMPA03

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

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

9 EN6114V5-7 1 BOLT

10 ASNA2529-5 1 NUT

11 EN6114V6-13 1 BOLT

12 ASNA2529-6 1 NUT

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: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

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

subsequent referenced NTM tasks:

- NTM 51-10-08

- NTM 51-10-01

(3) Special Tools

None

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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This Page Intentionally Left Blank

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 576115-832-801-001 - Do an HFEC Inspection of FR40 Lower Wing Junction Fastener

Holes

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 refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

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 mandated or expected to be mandated 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.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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Task Associated Data

**CONF 001

Zone

510 610

Access

Door 512AB 512BB 513AB 612AB 612BB 613AB

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

**CONF 002

Zone

510 610

Access

Door 512AB 512BB 513AB 612AB 612BB 613AB

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

**CONF 003

Zone

510 610

Access

Door 512AB 512BB 513AB 612AB 612BB 613AB

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 3.75

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 576115-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

06-31-53, Page Block 001

06-41-00, Page Block 001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-40-13

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(a) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.

(d) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Materials List (CML).

(e) Apply special protection in accordance with SRM 51-40-13.

(2) Subtask 576115-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 576115-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

06-31-53, Page Block 001

06-41-00, Page Block 001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-40-13

(a) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.

(d) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Materials List (CML).

(e) Apply special protection in accordance with SRM 51-40-13.

(2) Subtask 576115-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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**CONF 003

(1) Subtask 576115-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

06-31-53, Page Block 001

06-41-00, Page Block 001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-40-13

(a) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.

(d) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Materials List (CML).

(e) Apply special protection in accordance with SRM 51-40-13.

(2) Subtask 576115-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 576115-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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(a) The following items 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).

- 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 is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

Block 301.

(c) Put access platforms in position at zones 510 and 610.

(d) Open main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Open wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(f) If necessary, remove the left and right air conditioning ducts on FR39, refer to AMM

36-11-00, Page Block 401.

**CONF 002

(1) Subtask 576115-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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(a) The following items 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).

- 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 is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

Block 301.

(c) Put access platforms in position at zones 510 and 610.

(d) Open main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Open wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(f) If necessary, remove the left and right air conditioning ducts on FR39, refer to AMM

36-11-00, Page Block 401.

**CONF 003

(1) Subtask 576115-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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SERVICE BULLETIN

(a) The following items 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).

- 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 is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

Block 301.

(c) Put access platforms in position at zones 510 and 610.

(d) Open main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Open wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(f) If necessary, remove the left and right air conditioning ducts on FR39, refer to AMM

36-11-00, Page Block 401.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 576115-832-009-001 - Do an HFEC Inspection around fasteners at LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Non Destructive Test Manual (NTM) 51-10-08

Structural Repair Manual (SRM) 51-40-13

Fig. A-FBAAA

HFEC Inspection of the Fasteners

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in the planning information paragraph E.(2) Table 1.

NOTE: Before doing HFEC inspection, remove the sealant around fastener

heads with:

Non Aqueous

Cleaner - General

08BAA9 As required

(a) Do an HFEC inspection around FR40 lower junction fasteners.

Refer to NTM 51-10-08

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

1 If no crack is found

a Renew special protection in accordance with SRM 51-40-13.

b Repeat the inspection at the interval given in the planning information

paragraph E.(2) Table 1.

2 If crack is found

a Contact Airbus before the next flight.

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(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(2) Subtask 576115-832-002-001 - Do an HFEC Inspection around fasteners at RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Non Destructive Test Manual (NTM) 51-10-08

Structural Repair Manual (SRM) 51-40-13

Fig. A-FBAAA

HFEC Inspection of the Fasteners

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in the planning information paragraph E.(2) Table 1.

NOTE: Before doing HFEC inspection, remove sealant around fastener heads

with:

Non Aqueous

Cleaner - General

08BAA9 As required

(a) Do an HFEC inspection around FR40 lower junction fasteners.

Refer to NTM 51-10-08

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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1 If no crack is found

a Renew special protection in accordance with SRM 51-40-13.

b Repeat the inspection at the interval given in the planning information

paragraph E.(2) Table 1.

2 If crack is found

a Contact Airbus before the next flight.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

**CONF 002

(1) Subtask 576115-832-009-001 - Do an HFEC Inspection around fasteners at LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Non Destructive Test Manual (NTM) 51-10-08

Structural Repair Manual (SRM) 51-40-13

Fig. A-FBAAA

HFEC Inspection of the Fasteners

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in the planning information paragraph E.(2) Table 1.

NOTE: Before doing HFEC inspection, remove the sealant around fastener

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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SERVICE BULLETIN

heads with:

Non Aqueous

Cleaner - General

08BAA9 As required

(a) Do an HFEC inspection around FR40 lower junction fasteners.

Refer to NTM 51-10-08

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

1 If no crack is found

a Renew special protection in accordance with SRM 51-40-13.

b Repeat the inspection at the interval given in the planning information

paragraph E.(2) Table 1.

2 If crack is found

a Contact Airbus before the next flight.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(2) Subtask 576115-832-002-001 - Do an HFEC Inspection around fasteners at RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Non Destructive Test Manual (NTM) 51-10-08

Structural Repair Manual (SRM) 51-40-13

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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References

Fig. A-FBAAA

HFEC Inspection of the Fasteners

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in the planning information paragraph E.(2) Table 1.

NOTE: Before doing HFEC inspection, remove sealant around fastener heads

with:

Non Aqueous

Cleaner - General

08BAA9 As required

(a) Do an HFEC inspection around FR40 lower junction fasteners.

Refer to NTM 51-10-08

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

1 If no crack is found

a Renew special protection in accordance with SRM 51-40-13.

b Repeat the inspection at the interval given in the planning information

paragraph E.(2) Table 1.

2 If crack is found

a Contact Airbus before the next flight.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

**CONF 003

(1) Subtask 576115-832-009-001 - Do an HFEC Inspection around fasteners at LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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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

Non Aqueous Cleaner -

General

08BAA9 As required

References

Non Destructive Test Manual (NTM) 51-10-08

Structural Repair Manual (SRM) 51-40-13

Fig. A-FBAAA

HFEC Inspection of the Fasteners

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in the planning information paragraph E.(2) Table 1.

NOTE: Before doing HFEC inspection, remove the sealant around fastener

heads with:

Non Aqueous

Cleaner - General

08BAA9 As required

(a) Do an HFEC inspection around FR40 lower junction fasteners.

Refer to NTM 51-10-08

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

1 If no crack is found

a Renew special protection in accordance with SRM 51-40-13.

b Repeat the inspection at the interval given in the planning information

paragraph E.(2) Table 1.

2 If crack is found

a Contact Airbus before the next flight.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 33

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(2) Subtask 576115-832-002-001 - Do an HFEC Inspection around fasteners at RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Non Destructive Test Manual (NTM) 51-10-08

Structural Repair Manual (SRM) 51-40-13

Fig. A-FBAAA

HFEC Inspection of the Fasteners

Sheet 01

Sheet 02

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in the planning information paragraph E.(2) Table 1.

NOTE: Before doing HFEC inspection, remove sealant around fastener heads

with:

Non Aqueous

Cleaner - General

08BAA9 As required

(a) Do an HFEC inspection around FR40 lower junction fasteners.

Refer to NTM 51-10-08

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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1 If no crack is found

a Renew special protection in accordance with SRM 51-40-13.

b Repeat the inspection at the interval given in the planning information

paragraph E.(2) Table 1.

2 If crack is found

a Contact Airbus before the next flight.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 576115-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 36-11-00, Page Block 401

This Service Bulletin requires the accomplishment of the following Tests which are given

in subtasks included in the topic Close-up. The manhours for the tests are included in

the referenced Service Bulletin subtasks.

- Test after installation of left and right air conditioning ducts (if removed), refer to

AMM 36-11-00, Page Block 401.

**CONF 002

(1) Subtask 576115-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 36-11-00, Page Block 401

This Service Bulletin requires the accomplishment of the following Tests which are given

in subtasks included in the topic Close-up. The manhours for the tests are included in

the referenced Service Bulletin subtasks.

- Test after installation of left and right air conditioning ducts (if removed), refer to

AMM 36-11-00, Page Block 401.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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**CONF 003

(1) Subtask 576115-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 36-11-00, Page Block 401

This Service Bulletin requires the accomplishment of the following Tests which are given

in subtasks included in the topic Close-up. The manhours for the tests are included in

the referenced Service Bulletin subtasks.

- Test after installation of left and right air conditioning ducts (if removed), refer to

AMM 36-11-00, Page Block 401.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 576115-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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

equipment.

(b) If removed, install left and right air conditioning ducts, refer to AMM 36-11-00, Page

Block 401.

(c) Close wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(d) Close main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Remove the access platform(s).

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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 36

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**CONF 002

(1) Subtask 576115-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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

equipment.

(b) If removed, install left and right air conditioning ducts, refer to AMM 36-11-00, Page

Block 401.

(c) Close wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(d) Close main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Remove the access platform(s).

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

**CONF 003

(1) Subtask 576115-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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

equipment.

(b) If removed, install left and right air conditioning ducts, refer to AMM 36-11-00, Page

Block 401.

(c) Close wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(d) Close main landing gear doors, refer to AMM 32-12-11, Page Block 301.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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(e) Remove the access platform(s).

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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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SERVICE BULLETIN

Task 576115-832-803-001 - Do a Rototest Inspection of FR40 Lower Wing Junction Fastener

Holes

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY

INSTALLED ON THE LANDING GEAR. THIS PREVENTS UNWANTED

MOVEMENT OF THE LANDING GEAR.

MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT

AVAILABLE.

ISOLATE ALL THE AIRCRAFT ELECTRICAL CIRCUITS. UNWANTED

ELECTRICAL POWER CAN BE DANGEROUS.

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 refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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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 mandated or expected to be mandated 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.

Task Associated Data

**CONF 001

Zone

510 610

Access

Door 512AB 512BB 513AB 612AB 612BB 613AB

Manpower

TOTAL MANHOURS 11.50

ELAPSED TIME (HOURS) 5.75

**CONF 002

Zone

141 142 510 610

Access

Door 147AZ 148AZ 512AB 512BB 513AB 612AB 612BB 613AB

Manpower

TOTAL MANHOURS 43.00

ELAPSED TIME (HOURS) 21.50

**CONF 003

Zone

141 142 510 610

Access

Door 147AZ 148AZ 512AB 512BB 513AB 612AB 612BB 613AB

Manpower

TOTAL MANHOURS 43.00

ELAPSED TIME (HOURS) 21.50

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**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 576115-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

06-31-53, Page Block 001

06-41-00, Page Block 001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-24-00

51-40-00

51-40-12

51-40-13

51-40-20

51-40-30

(a) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.

(d) Remove and install fasteners in accordance with SRM 51-40-20.

(e) Obtain alternative and substitute fastener data, in accordance with SRM 51-40-30.

(f) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) Apply sealant in accordance with SRM 51-24-00.

(i) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Material List (CML).

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

related unit.

(k) Do the painting in accordance with SRM 51-40-12.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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(l) Apply special protection in accordance with SRM 51-40-13.

(2) Subtask 576115-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 576115-910-002-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

06-31-53, Page Block 001

06-41-00, Page Block 001

28-00-00, Page Block 301

Consumable Material List (CML)

Non Destructive Test Manual (NTM) 51-10-01

51-10-08

Structural Repair Manual (SRM) 51-24-00

51-40-00

51-40-12

51-40-13

51-40-20

51-40-30

(a) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.

(d) Remove and install fasteners in accordance with SRM 51-40-20.

(e) Obtain alternative and substitute fastener data, in accordance with SRM 51-40-30.

(f) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) Apply sealant in accordance with SRM 51-24-00.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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(i) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Material List (CML).

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

related unit.

(k) Do the painting in accordance with SRM 51-40-12.

(l) Apply special protection in accordance with SRM 51-40-13.

(m) Obey the instruction of the fuel safety procedure, refer to AMM 28-00-00, Page

Block 301, and make sure that the ventilation of the center tank is correct.

(2) Subtask 576115-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 576115-910-002-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

06-31-53, Page Block 001

06-41-00, Page Block 001

28-00-00, Page Block 301

Consumable Material List (CML)

Non Destructive Test Manual (NTM) 51-10-01

51-10-08

Structural Repair Manual (SRM) 51-24-00

51-40-00

51-40-12

51-40-13

51-40-20

51-40-30

(a) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-00, Page Block 001.

(d) Remove and install fasteners in accordance with SRM 51-40-20.

(e) Obtain alternative and substitute fastener data, in accordance with SRM 51-40-30.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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(f) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) Apply sealant in accordance with SRM 51-24-00.

(i) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Material List (CML).

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

related unit.

(k) Do the painting in accordance with SRM 51-40-12.

(l) Apply special protection in accordance with SRM 51-40-13.

(m) Obey the instruction of the fuel safety procedure, refer to AMM 28-00-00, Page

Block 301, and make sure that the ventilation of the center tank is correct.

(2) Subtask 576115-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 576115-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 44

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@A300-600

SERVICE BULLETIN

(a) The following items 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).

- 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 is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

Block 301.

(c) Put access platforms in position at zones 510 and 610.

(d) Open main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Open wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(f) If necessary, remove the left and right air conditioning ducts on FR39, refer to AMM

36-11-00, Page Block 401.

**CONF 002

(1) Subtask 576115-941-002-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

28-00-00, Page Block 301

28-10-00, Page Block 301

28-11-29, Page Block 401

28-25-00, Page Block 301

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 45

5

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

SERVICE BULLETIN

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY

INSTALLED ON THE LANDING GEAR.

MAKE CERTAIN THAT FIRE FIGHTING EQUIPMENT IS AVAILABLE

AND ADEQUATE.

DO NOT CONNECT GROUND POWER OR SWITCH ON ANY

AIRCRAFT ELECTRICAL SYSTEM UNTIL THE FUEL TANKS HAVE

BEEN COMPLETELY DRAINED AND VENTED.

OBEY THE FUEL SERVICING SAFETY INSTRUCTIONS.

(a) The following items 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).

- 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 is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

Block 301.

(c) Put access platforms in position at zones 510 and 610.

(d) Defuel the center tank, refer to AMM 28-25-00, Page Block 301.

NOTE: Defuel the center tank for:

- Remove the two fasteners to make possible access of the three

holes to be inspected.

- In case of finding, defueling will be necessary.

(e) Degas and ventilate fuel tank, refer to AMM 28-00-00, Page Block 301 and AMM

28-10-00, Page Block 301.

(f) Open main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(g) Open access doors 147AZ and 148AZ, refer to AMM 28-11-29, Page Block 401.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 46

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@A300-600

SERVICE BULLETIN

(h) Open wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(i) If necessary, remove the left and right air conditioning ducts on FR39, refer to AMM

36-11-00, Page Block 401.

**CONF 003

(1) Subtask 576115-941-002-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

28-00-00, Page Block 301

28-10-00, Page Block 301

28-11-29, Page Block 401

28-25-00, Page Block 301

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY

INSTALLED ON THE LANDING GEAR.

MAKE CERTAIN THAT FIRE FIGHTING EQUIPMENT IS AVAILABLE

AND ADEQUATE.

DO NOT CONNECT GROUND POWER OR SWITCH ON ANY

AIRCRAFT ELECTRICAL SYSTEM UNTIL THE FUEL TANKS HAVE

BEEN COMPLETELY DRAINED AND VENTED.

OBEY THE FUEL SERVICING SAFETY INSTRUCTIONS.

(a) The following items 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).

- 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 is available.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 47

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

SERVICE BULLETIN

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

Block 301.

(c) Put access platforms in position at zones 510 and 610.

(d) Defuel the center tank, refer to AMM 28-25-00, Page Block 301.

NOTE: Defuel the center tank for:

- Remove the two fasteners to make possible access of the three

holes to be inspected.

- In case of finding, defueling will be necessary.

(e) Degas and ventilate fuel tank, refer to AMM 28-00-00, Page Block 301 and AMM

28-10-00, Page Block 301.

(f) Open main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(g) Open access doors 147AZ and 148AZ, refer to AMM 28-11-29, Page Block 401.

(h) Open wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(i) If necessary, remove the left and right air conditioning ducts on FR39, refer to AMM

36-11-00, Page Block 401.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 576115-000-004-001 - Remove the Fasteners from LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 48

5

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

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Structural Repair Manual (SRM) 51-40-20

Fig. A-FBCAA

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Remove:

Refer to Fig. A-FBCAA

Refer to SRM 51-40-20

1 Bolt Item (1) Discard

1 Nut Item (2) Discard

2 Bolt Item (3) Discard

2 Nut Item (4) Discard

(b) Clean the area to be inspected with:

Non Aqueous

Cleaner - General

08BAA9 As required

(2) Subtask 576115-000-003-001 - Remove the Fasteners from RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 49

5

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

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Structural Repair Manual (SRM) 51-40-20

Fig. A-FBCAA

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Remove:

Refer to Fig. A-FBCAA

Refer to SRM 51-40-20

1 Bolt Item (1) Discard

1 Nut Item (2) Discard

2 Bolt Item (3) Discard

2 Nut Item (4) Discard

(b) Clean the area to be inspected with:

Non Aqueous

Cleaner - General

08BAA9 As required

(3) Subtask 576115-832-008-001 - Do a Rototest Inspection of Fasteners Holes at LH

Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 50

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBBAA

Rototest Inspection of the Fasteners

Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) Measure the diameter of the FR40 lower junction fastener holes.

Refer to Fig. A-FBBAA

Refer to Fig. A-FFAAA

1 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) and are not in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Contact Airbus before the next flight.

2 If the holes diameters are in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-004 001 Install New Fasteners on

LH Side .

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

3 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) but are in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 51

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@A300-600

SERVICE BULLETIN

<2> If no crack is found

<a> Do SUBTASK 576115-400-004 001 Install New Fasteners on

LH Side .

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(4) Subtask 576115-832-007-001 - Do a Rototest Inspection of Fasteners Holes at RH

Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

Fig. A-FBBAA

Rototest Inspection of the Fasteners

Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) Measure the diameter of the FR40 lower junction fastener holes.

Refer to Fig. A-FBBAA

Refer to Fig. A-FFAAA

1 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) and are not in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Contact Airbus before the next flight.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 52

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

SERVICE BULLETIN

2 If the holes diameters are in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-003 001 Install New Fasteners on

RH Side

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

3 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) but are in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-003 001 Install New Fasteners on

RH Side

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(5) Subtask 576115-400-004-001 - Install New Fasteners on LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 53

5

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

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

Polysulfide Sealant - Fuel

Tank Brushable

06ABA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-40-20

51-40-30

Fig. A-FBCAA

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Install:

Refer to Fig. A-FBCAA

Refer to SRM 51-40-20 and SRM 51-40-30

1 Bolt MS21250-10022 Item 1

1 Nut NSA5057-10 Item 2

2 Bolt MS21250-09020 Item 3

2 Nut NSA5057-9 Item 4

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 54

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@A300-600

SERVICE BULLETIN

(b) Apply:

Refer to SRM 51-24-00

Polysulfide Sealant

- Fuel Tank

Brushable

06ABA1 As required

(c) Protect the fasteners heads and nuts with:

Polyurethane Paint 04EAC2 As required

Top Coat

Polyurethane

04JME4 As required

(6) Subtask 576115-400-003-001 - Install New Fasteners on RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

Polysulfide Sealant - Fuel

Tank Brushable

06ABA1 As required

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 55

5

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

SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-24-00

51-40-20

51-40-30

Fig. A-FBCAA

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Install:

Refer to Fig. A-FBCAA

Refer to SRM 51-40-20 and SRM 51-40-30

1 Bolt MS21250-10022 Item 1

1 Nut NSA5057-10 Item 2

2 Bolt MS21250-09020 Item 3

2 Nut NSA5057-9 Item 4

(b) Apply:

Refer to SRM 51-24-00

Polysulfide Sealant

- Fuel Tank

Brushable

06ABA1 As required

(c) Protect the fasteners heads and nuts with:

Polyurethane Paint 04EAC2 As required

Top Coat

Polyurethane

04JME4 As required

**CONF 002

(1) Subtask 576115-000-004-002 - Remove the Fasteners from LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

141 Access Door 147AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 56

5

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

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Structural Repair Manual (SRM) 51-40-20

Fig. A-FBCAB

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Remove:

Refer to Fig. A-FBCAB

Refer to SRM 51-40-20

1 Bolt Item (5) Retain

1 Nut Item (6) Retain

1 Bolt Item (7) Retain

1 Nut Item (8) Retain

(b) Remove:

Refer to Fig. A-FBCAB

Refer to SRM 51-40-20

1 Bolt Item (1) Discard

1 Nut Item (2) Discard

2 Bolt Item (3) Discard

2 Nut Item (4) Discard

(c) Clean the area to be inspected with:

Non Aqueous

Cleaner - General

08BAA9 As required

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 57

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

SERVICE BULLETIN

(2) Subtask 576115-000-003-002 - Remove the Fasteners from RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

142 Access Door 148AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Structural Repair Manual (SRM) 51-40-20

Fig. A-FBCAB

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Remove:

Refer to Fig. A-FBCAB

Refer to SRM 51-40-20

1 Bolt Item (5) Retain

1 Nut Item (6) Retain

1 Bolt Item (7) Retain

1 Nut Item (8) Retain

(b) Remove:

Refer to Fig. A-FBCAB

Refer to SRM 51-40-20

1 Bolt Item (1) Discard

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 58

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@A300-600

SERVICE BULLETIN

1 Nut Item (2) Discard

2 Bolt Item (3) Discard

2 Nut Item (4) Discard

(c) Clean the area to be inspected with:

Non Aqueous

Cleaner - General

08BAA9 As required

(3) Subtask 576115-832-008-001 - Do a Rototest Inspection of Fasteners Holes at LH

Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

Fig. A-FBBAA

Rototest Inspection of the Fasteners

Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) Measure the diameter of the FR40 lower junction fastener holes.

Refer to Fig. A-FBBAA

Refer to Fig. A-FFAAA

1 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) and are not in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Contact Airbus before the next flight.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 59

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

SERVICE BULLETIN

2 If the holes diameters are in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-004 002 Install New Fasteners on

LH Side .

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

3 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) but are in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-004 002 Install New Fasteners on

LH Side .

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(4) Subtask 576115-832-007-001 - Do a Rototest Inspection of Fasteners Holes at RH

Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 60

5

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

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

Fig. A-FBBAA

Rototest Inspection of the Fasteners

Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) Measure the diameter of the FR40 lower junction fastener holes.

Refer to Fig. A-FBBAA

Refer to Fig. A-FFAAA

1 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) and are not in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Contact Airbus before the next flight.

2 If the holes diameters are in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-003 002 Install New Fasteners on

RH Side

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 61

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3 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) but are in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-003 002 Install New Fasteners on

RH Side

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(5) Subtask 576115-400-004-002 - Install New Fasteners on LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

141 Access Door 147AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

5 EN6114V5-15 1 BOLT

6 ASNA2529-5 1 NUT

7 EN6114V6-15 1 BOLT

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 62

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 ASNA2529-6 1 NUT

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

Polysulfide Sealant - Fuel

Tank Brushable

06ABA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-40-20

51-40-30

Fig. A-FBCAB

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Install:

Refer to Fig. A-FBCAB

Refer to SRM 51-40-20 and SRM 51-40-30

1 Bolt MS21250-10022 Item 1

1 Nut NSA5057-10 Item 2

2 Bolt MS21250-09020 Item 3

2 Nut NSA5057-9 Item 4

(b) Install:

1 Bolt EN6114V5-15 Item 5

1 Nut ASNA2529-5 Item 6

1 Bolt EN6114V6-15 Item 7

1 Nut ASNA2529-6 Item 8

(c) Apply:

Refer to SRM 51-24-00

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 63

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SERVICE BULLETIN

Polysulfide Sealant

- Fuel Tank

Brushable

06ABA1 As required

(d) Protect the fasteners heads and nuts with:

Polyurethane Paint 04EAC2 As required

Top Coat

Polyurethane

04JME4 As required

(6) Subtask 576115-400-003-002 - Install New Fasteners on RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

142 Access Door 148AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

5 EN6114V5-15 1 BOLT

6 ASNA2529-5 1 NUT

7 EN6114V6-15 1 BOLT

8 ASNA2529-6 1 NUT

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 64

5

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@A300-600

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant - Fuel

Tank Brushable

06ABA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-40-20

51-40-30

Fig. A-FBCAB

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Install:

Refer to Fig. A-FBCAB

Refer to SRM 51-40-20 and SRM 51-40-30

1 Bolt MS21250-10022 Item 1

1 Nut NSA5057-10 Item 2

2 Bolt MS21250-09020 Item 3

2 Nut NSA5057-9 Item 4

(b) Install:

1 Bolt EN6114V5-15 Item 5

1 Nut ASNA2529-5 Item 6

1 Bolt EN6114V6-15 Item 7

1 Nut ASNA2529-6 Item 8

(c) Apply:

Refer to SRM 51-24-00

Polysulfide Sealant

- Fuel Tank

Brushable

06ABA1 As required

(d) Protect the fasteners heads and nuts with:

Polyurethane Paint 04EAC2 As required

Top Coat

Polyurethane

04JME4 As required

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 65

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SERVICE BULLETIN

**CONF 003

(1) Subtask 576115-000-004-003 - Remove the Fasteners from LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

141 Access Door 147AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Structural Repair Manual (SRM) 51-40-20

Fig. A-FBCAC

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Remove:

Refer to Fig. A-FBCAC

Refer to SRM 51-40-20

1 Bolt Item (9) Retain

1 Nut Item (10) Retain

1 Bolt Item (11) Retain

1 Nut Item (12) Retain

(b) Remove:

Refer to Fig. A-FBCAC

Refer to SRM 51-40-20

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 66

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SERVICE BULLETIN

1 Bolt Item (1) Discard

1 Nut Item (2) Discard

2 Bolt Item (3) Discard

2 Nut Item (4) Discard

(c) Clean the area to be inspected with:

Non Aqueous

Cleaner - General

08BAA9 As required

(2) Subtask 576115-000-003-003 - Remove the Fasteners from RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

142 Access Door 148AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

References

Structural Repair Manual (SRM) 51-40-20

Fig. A-FBCAC

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Remove:

Refer to Fig. A-FBCAC

Refer to SRM 51-40-20

1 Bolt Item (9) Retain

1 Nut Item (10) Retain

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 67

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@A300-600

SERVICE BULLETIN

1 Bolt Item (11) Retain

1 Nut Item (12) Retain

(b) Remove:

Refer to Fig. A-FBCAC

Refer to SRM 51-40-20

1 Bolt Item (1) Discard

1 Nut Item (2) Discard

2 Bolt Item (3) Discard

2 Nut Item (4) Discard

(c) Clean the area to be inspected with:

Non Aqueous

Cleaner - General

08BAA9 As required

(3) Subtask 576115-832-008-001 - Do a Rototest Inspection of Fasteners Holes at LH

Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

Fig. A-FBBAA

Rototest Inspection of the Fasteners

Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 68

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(a) Measure the diameter of the FR40 lower junction fastener holes.

Refer to Fig. A-FBBAA

Refer to Fig. A-FFAAA

1 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) and are not in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Contact Airbus before the next flight.

2 If the holes diameters are in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-004 003 Install New Fasteners on

LH Side .

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

3 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) but are in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-004 003 Install New Fasteners on

LH Side .

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 69

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SERVICE BULLETIN

(4) Subtask 576115-832-007-001 - Do a Rototest Inspection of Fasteners Holes at RH

Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

Fig. A-FBBAA

Rototest Inspection of the Fasteners

Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) Measure the diameter of the FR40 lower junction fastener holes.

Refer to Fig. A-FBBAA

Refer to Fig. A-FFAAA

1 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) and are not in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Contact Airbus before the next flight.

2 If the holes diameters are in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 70

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<2> If no crack is found

<a> Do SUBTASK 576115-400-003 003 Install New Fasteners on

RH Side

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

3 If the holes diameters are not in tolerance of Fig. A-FBBAA Sheet 03 Table 1

(nominal diameter) but are in tolerance of Fig. A-FBBAA Sheet 03 Table 2

(first and second oversize)

a Do a rototest inspection of FR40 lower junction fastener holes, refer to

NTM 51-10-01.

<1> If crack is found

<a> Contact Airbus before next flight.

<2> If no crack is found

<a> Do SUBTASK 576115-400-003 003 Install New Fasteners on

RH Side

And

<b> Repeat the inspection at the interval given in the planning

information paragraph E.(2) Table 2.

(b) Send inspection report to Airbus, refer to Fig. A-FRAAA.

(5) Subtask 576115-400-004-003 - Install New Fasteners on LH Side

Work Zones and Access Panels

Zone Access/Work location

510 Access Door 512AB, Door 512BB, Door 513AB

Work location Frame 40

141 Access Door 147AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 71

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Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

9 EN6114V5-7 1 BOLT

10 ASNA2529-5 1 NUT

11 EN6114V6-13 1 BOLT

12 ASNA2529-6 1 NUT

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

Polysulfide Sealant - Fuel

Tank Brushable

06ABA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-40-20

51-40-30

Fig. A-FBCAC

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Install:

Refer to Fig. A-FBCAC

Refer to SRM 51-40-20 and SRM 51-40-30

1 Bolt MS21250-10022 Item 1

1 Nut NSA5057-10 Item 2

2 Bolt MS21250-09020 Item 3

2 Nut NSA5057-9 Item 4

(b) Install:

1 Bolt EN6114V5-7 Item 9

1 Nut ASNA2529-5 Item 10

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 72

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1 Bolt EN6114V6-13 Item 11

1 Nut ASNA2529-6 Item 12

(c) Apply:

Refer to SRM 51-24-00

Polysulfide Sealant

- Fuel Tank

Brushable

06ABA1 As required

(d) Protect the fasteners heads and nuts with:

Polyurethane Paint 04EAC2 As required

Top Coat

Polyurethane

04JME4 As required

(6) Subtask 576115-400-003-003 - Install New Fasteners on RH Side

Work Zones and Access Panels

Zone Access/Work location

610 Access Door 612AB, Door 612BB, Door 613AB

Work location Frame 40

142 Access Door 148AZ

Work location Frame 40

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21250-10022 1 BOLT

2 NSA5057-10 1 NUT

3 MS21250-09020 2 BOLT

4 NSA5057-9 2 NUT

9 EN6114V5-7 1 BOLT

10 ASNA2529-5 1 NUT

11 EN6114V6-13 1 BOLT

12 ASNA2529-6 1 NUT

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 73

5

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Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polyurethane Paint 04EAC2 As required

Top Coat Polyurethane 04JME4 As required

Polysulfide Sealant - Fuel

Tank Brushable

06ABA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-40-20

51-40-30

Fig. A-FBCAC

Removal/Installation of Fasteners

Sheet 01

Sheet 02

(a) Install:

Refer to Fig. A-FBCAC

Refer to SRM 51-40-20 and SRM 51-40-30

1 Bolt MS21250-10022 Item 1

1 Nut NSA5057-10 Item 2

2 Bolt MS21250-09020 Item 3

2 Nut NSA5057-9 Item 4

(b) Install:

1 Bolt EN6114V5-7 Item 9

1 Nut ASNA2529-5 Item 10

1 Bolt EN6114V6-13 Item 11

1 Nut ASNA2529-6 Item 12

(c) Apply:

Refer to SRM 51-24-00

Polysulfide Sealant

- Fuel Tank

Brushable

06ABA1 As required

(d) Protect the fasteners heads and nuts with:

Polyurethane Paint 04EAC2 As required

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 74

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Top Coat

Polyurethane

04JME4 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 576115-700-002-002 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 36-11-00, Page Block 401

This Service Bulletin requires the accomplishment of the following Tests which are given

in subtasks included in the topic Close-up. The manhours for the tests are included in

the referenced Service Bulletin subtasks.

- Test after installation of left and right air conditioning ducts (if removed), refer to

AMM 36-11-00, Page Block 401.

**CONF 002

(1) Subtask 576115-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 28-11-00, Page Block 501

28-11-29, Page Block 401

36-11-00, Page Block 401

This Service Bulletin requires the accomplishment of the following Tests which are given

in subtasks included in the topic Close-up. The manhours for the tests are included in

the referenced Service Bulletin subtasks.

- Test after installation of left and right air conditioning ducts (if removed), refer to

AMM 36-11-00, Page Block 401.

- Test after installation of the manhole cover, refer to AMM 28-11-29, Page Block

401.

- Test after the refueling of the center tank, refer to AMM 28-11-00, Page Block 501.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 75

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SERVICE BULLETIN

**CONF 003

(1) Subtask 576115-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 28-11-00, Page Block 501

28-11-29, Page Block 401

36-11-00, Page Block 401

This Service Bulletin requires the accomplishment of the following Tests which are given

in subtasks included in the topic Close-up. The manhours for the tests are included in

the referenced Service Bulletin subtasks.

- Test after installation of left and right air conditioning ducts (if removed), refer to

AMM 36-11-00, Page Block 401.

- Test after installation of the manhole cover, refer to AMM 28-11-29, Page Block

401.

- Test after the refueling of the center tank, refer to AMM 28-11-00, Page Block 501.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 576115-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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

equipment.

(b) If removed, install left and right air conditioning ducts, refer to AMM 36-11-00, Page

Block 401.

(c) Close wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(d) Close main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Remove the access platform(s).

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 76

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

**CONF 002

(1) Subtask 576115-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 28-11-00, Page Block 501

28-11-29, Page Block 401

WARNING: MAKE CERTAIN THAT FIRE FIGHTING EQUIPMENT IS AVAILABLE

AND ADEQUATE.

OBEY THE FUEL SERVICING SAFETY INSTRUCTIONS.

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

equipment.

(b) If opened, close access doors 147AZ and 148AZ, refer to AMM 28-11-29, Page

Block 401.

(c) Refuel the center tank, refer to AMM 28-11-00, Page Block 501.

(2) Subtask 576115-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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

equipment.

(b) If removed, install left and right air conditioning ducts, refer to AMM 36-11-00, Page

Block 401.

(c) Close wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(d) Close main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Remove the access platform(s).

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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 77

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@A300-600

SERVICE BULLETIN

**CONF 003

(1) Subtask 576115-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 28-11-00, Page Block 501

28-11-29, Page Block 401

WARNING: MAKE CERTAIN THAT FIRE FIGHTING EQUIPMENT IS AVAILABLE

AND ADEQUATE.

OBEY THE FUEL SERVICING SAFETY INSTRUCTIONS.

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

equipment.

(b) If opened, close access doors 147AZ and 148AZ, refer to AMM 28-11-29, Page

Block 401.

(c) Refuel the center tank, refer to AMM 28-11-00, Page Block 501.

(2) Subtask 576115-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

32-12-11, Page Block 301

36-11-00, Page Block 401

57-41-41, Page Block 401

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

equipment.

(b) If removed, install left and right air conditioning ducts, refer to AMM 36-11-00, Page

Block 401.

(c) Close wing access doors 512AB, 512BB, 513AB, 612AB, 612BB, 613AB, refer to

AMM 06-41-57, Page Block 001 and AMM 57-41-41, Page Block 401.

(d) Close main landing gear doors, refer to AMM 32-12-11, Page Block 301.

(e) Remove the access platform(s).

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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 78

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**CONF ALL

B

FR40

RH SHOWN

LH SYMMETRICAL

A

B

A Z140

A

A

B

D_SB_576115_5_BAAA_01_02

Figure A-FBAAA - Sheet 01

HFEC Inspection of the Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 79

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**CONF ALL

B B

INSPECTION AREA

NOTE:

B

B

WING SIDE INBOARD SIDE

RIB1

A A

D_SB_576115_5_BAAA_02_02

Figure A-FBAAA - Sheet 02

HFEC Inspection of the Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 80

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**CONF ALL

B

FR40

RH SHOWN

LH SYMMETRICAL

A

B

A Z140

A

A

B

D_SB_576115_5_BBAA_01_02

Figure A-FBBAA - Sheet 01

Rototest Inspection of the Fasteners Holes

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 81

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SERVICE BULLETIN

**CONF ALL

FASTENERS HOLES

TO BE INSPECTED

RIB1

WING SIDE

INBOARD SIDE

01

NOTE:

01 FOR THE HOLE DIAMETERS REFER TO FIGURE A−FBBAA SHEET03

A A

D_SB_576115_5_BBAA_02_02

Figure A-FBBAA - Sheet 02

Rototest Inspection of the Fasteners Holes

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 82

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SERVICE BULLETIN

**CONF ALL

NUMBER

BOLT DIAMETER

16

14

12

10

9

8

7

6

5

4

3

mm

MAXI

in

STANDARD HOLE DIAMETERS

SPECIAL CLEARANCE FIT

mm

MINI

in

5.287 0.2081 5.012 0.1973

6.811 0.2681 6.536 0.2573

8.399 0.3307 8.125 0.3199

9.986 0.3931 9.711 0.3823

11.574 0.4557 11.300 0.4449

13.161 0.5181 12.887 0.5074

14.736 0.5801 14.461 0.5693

16.324 0.6427 16.049 0.6318

19.499 0.7677 19.224 0.7568

22.674 0.8927 22.399 0.8818

25.849 1.0177 25.574 1.0068

NUMBER

BOLT DIAMETER

14

12

10

9

8

7

6

5

4

mm

MAXI

in

1ST OVERSIZE (NOMINAL DIA +0.4mm

 (1/64 in ))

mm

MINI

in

7.209 0.2838 6.933 0.2729

8.795 0.3462 8.522 0.3355

10.384 0.4088 10.109 0.3980

11.971 0.4713 11.696 0.4605

13.558 0.5338 13.283 0.5229

15.133 0.5958 14.859 0.5850

16.721 0.6583 16.446 0.6475

19.896 0.7833 19.621 0.7725

23.071 0.9083 22.796 0.8975

mm

MAXI

in mm

MINI

in

7.605 0.2994 7.330 0.2886

9.192 0.3619 8.918 0.3511

10.780 0.4244 10.505 0.4136

12.367 0.4869 12.092 0.4761

13.954 0.5494 13.680 0.5386

15.529 0.6114 15.255 0.6006

17.117 0.6739 16.842 0.6631

20.292 0.7989 20.017 0.7881

23.467 0.9239 23.192 0.9131

OVERSIZE HOLE DIAMETERS − SPECIAL CLEARANCE FIT

2ND OVERSIZE (NOMINAL DIA +0.8mm

(1/32 in ))

TABLE1 − NOMINAL HOLE DIAMETERS

TABLE2 − 1ST AND 2ND OVERSIZE HOLE DIAMETERS

D_SB_576115_5_BBAA_03_00

Figure A-FBBAA - Sheet 03

Rototest Inspection of the Fasteners Holes

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 83

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**CONF 001

B

FR40

RH SHOWN

LH SYMMETRICAL

A

B

A Z140

A

A

B

D_SB_576115_5_BCAA_01_02

Figure A-FBCAA - Sheet 01

Removal/Installation of Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 84

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**CONF 001

APPLY POLYSULFIDE SEALANT MAT. No 06ABA1

NOTE:

01

A A

1

2

(1)

(2)

(3)

(4)

3

4

WING SIDE INBOARD SIDE

01

02

01

02

02 PROTECT THE FASTENERS HEADS AND NUTS WITH PRIMER POLYURETHANE PAINT

MAT. No 04EAC2 AND TOP COAT POLYURETHANE MAT. No 04JME4

RIB1

D_SB_576115_5_BCAA_02_01

Figure A-FBCAA - Sheet 02

Removal/Installation of Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 85

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**CONF 002

B

FR40

RH SHOWN

LH SYMMETRICAL

A

B

A Z140

A

A

B

D_SB_576115_5_BCAB_01_01

Figure A-FBCAB - Sheet 01

Removal/Installation of Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 86

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SERVICE BULLETIN

**CONF 002

A A

1

2

(1)

(2)

(3)

(4)

3

4

WING SIDE INBOARD SIDE

01

02

01

02

APPLY POLYSULFIDE SEALANT MAT. No 06ABA1

NOTE:

01

02 PROTECT THE FASTENERS HEADS AND NUTS WITH PRIMER POLYURETHANE PAINT

MAT. No 04EAC2 AND TOP COAT POLYURETHANE MAT. No 04JME4

F

F

HEAD ON THE HIDDEN SIDE

F

HOLE

SYMBOL DESCRIPTION

BOLT

NUT

BOLT

NUT

(5)

(6)

(7)

(8)

NOTE

01

01

01

01

OLD

ITEM

NEW

ITEM

5

6

7

8

PN

EN6114V5−15

ASNA2529−5

EN6114V6−15

ASNA2529−6

RIB1

D_SB_576115_5_BCAB_02_00

Figure A-FBCAB - Sheet 02

Removal/Installation of Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 87

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**CONF 003

B

FR40

RH SHOWN

LH SYMMETRICAL

A

B

A Z140

A

A

B

D_SB_576115_5_BCAC_01_01

Figure A-FBCAC - Sheet 01

Removal/Installation of Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 88

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SERVICE BULLETIN

**CONF 003

A A

1

2

(1)

(2)

(3)

(4)

3

4

WING SIDE INBOARD SIDE

01

02

01

02

APPLY POLYSULFIDE SEALANT MAT. No 06ABA1

NOTE:

01

02 PROTECT THE FASTENERS HEADS AND NUTS WITH PRIMER POLYURETHANE PAINT

MAT. No 04EAC2 AND TOP COAT POLYURETHANE MAT. No 04JME4

HOLE

SYMBOL DESCRIPTION

BOLT

NUT

BOLT

F NUT

(9)

(10)

(11)

(12)

F

NOTE

01

01

01

01

HEAD ON THE HIDDEN SIDE

F

OLD

ITEM

NEW

ITEM

9

10

11

12

RIB1

PN

EN6114V5−7

ASNA2529−5

EN6114V6−13

ASNA2529−6

D_SB_576115_5_BCAC_02_00

Figure A-FBCAC - Sheet 02

Removal/Installation of Fasteners

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 89

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**CONF ALL

THRESHOLD GIVEN IN THE PLANNING INFORMATION

PARAGRAPH E.(2)

REFER TO TASK 576115−832−801−001

FASTENER HOLES (LH AND RH SIDES) AT THE

DO A SPECIAL DETAILED INSPECTION OFFR40

OR

ON /LOWER WING JUNCTION,

ON FASTENERS 1 TO 3 ON EACH A/C SIDE,

PERFORM FIRST HFEC INSPECTION

ON FITTING AROUND FASTENER HEADS AT THE

THRESHOLD GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2) TABLE 1

REFER TO SUBTASK 576115−832−002 FOR RHS

REFER TO SUBTASK 576115−832−009 FOR LHS

(TASK 576115−832−801−001)

REMOVE THE FASTENERS 1 TO 3

ON EACH A/C SIDE AT THE THRESHOLD

GIVEN IN THE PLANNING INFORMATION

PARAGRAPH E.(2) TABLE 2

REFER TO SUBTASK 576115−000−003 FOR RHS

REFER TO SUBTASK 576115−000−004 FOR LHS

(TASK 576115−832−803−001)

HOLES

DIAMETER IN TOLERANCE OF

SPECIAL CLEARANCE FIT FASTENER

(NOMINAL DIAMETER)

REFER TO SUBTASK

576115−832−007 FOR RHS

REFER TO SUBTASK

HOLES

DIAMETER IN TOLERANCE OF

SPECIAL CLEARANCE FIT FASTENER

(1st AND 2nd OVERSIZE DIAMETER)

REFER TO SUBTASK

576115−832−007 FOR RHS

REFER TO SUBTASK

576115−832−008 FOR LHS

PERFORM DETAILED (DET) INSPECTION AND ROTOTEST

INSPECTION OF THE FASTENERS HOLES

REFER TO SUBTASK 576115−832−007 FOR RHS

REFER TO SUBTASK 576115−832−008 FOR LHS

CRACKS

FOUND

CONTACT AIRBUS

BEFORE NEXT FLIGHT

INSTALL NEW FASTENER SAME

DIAMETER IN SPECIAL CLEARANCE

FIT FOR FASTENERS 1 TO 3

REFER TO SUBTASK 576115−400−003 FOR RHS

REFER TO SUBTASK 576115−400−004 FOR LHS

NO

REPEAT INSPECTION

AT THE INTERVAL GIVEN IN THE

PLANNING INFORMATION PARAGRAPH E.(2)

REFER TO TASK 576115−832−803−001

YES

CRACKS

FOUND NO

YES

CONTACT AIRBUS

BEFORE NEXT FLIGHT

NO

YES YES

QUESTION

ACTION

FINDING

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.

NO

CONTACT AIRBUS

BEFORE NEXT FLIGHT

REPEAT THE INSPECTION AT THE

INTERVAL GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2)

REFER TO TASK 576115−832−801−001

576115−832−008 FOR LHS

FR40 ON /LOWER WING JUNCTION, FR40

LOWER JUNCTION

D_SB_576115_5_FAAA_01_02

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 90

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**CONF ALL

YES

NO

LEFT SIDE

CRACK DETECTED

WITH HFEC INSPECTION

HOLES DIAMETER IN

TOLERANCE OF SPECIAL

CLEARANCE FIT FASTENER

HOLES DIAMETER IN TOLERANCE

OF SPECIAL CLEARANCE FIT

FASTENER (1st AND 2nd OVERSIZE)

CRACK DETECTED

WITH DET AND ROTOTEST

INSPECTION

YES

NO

RIGHT SIDE

YES

NO

YES

NO

YES

NO

YES

NO

YES

NO

YES

NO

INSPECTION REPORT

SERVICE BULLETIN No :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−57−6115

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES1

CENTER WING BOX (WB/LR)

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: Structure.sbinspectionresult@airbus.com SPECIAL DETAILED

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

(NOMINAL DIAMETER)

D_SB_576115_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 91

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This Page Intentionally Left Blank

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 92

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SERVICE BULLETIN

Appendix 01: Elapsed Time Assumption

**CONF ALL

For an explanation of the manhours and elapsed time, refer to the following Gantt Chart.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 1

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Appendix 01: Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−57−6115

01

02

GET ACCESS

DO A HFEC INSPECTION

CLOSE−UP

RH SIDE

DO A HFEC INSPECTION

LH SIDE

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

7.50

3.75

STEPS

2.00 1.00

0 3

1.50 1.50

1.50 1.50

2.50 1.25

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

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

1

1

2

:

:

SB ELAPSED TIME

(HOURS)

1 2

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

D_SB_576115_5_AAAA_01_01

Figure A-FAAAA - Sheet 01

Gantt Chart for HFEC Inspection

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 2

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Appendix 01: Elapsed Time Assumption

**CONF 001

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−57−6115

01

02

GET ACCESS

REMOVE THE FASTENERS

CLOSE−UP

RH SIDE

REMOVE THE FASTENERS

LH SIDE

DO A ROTOTEST

INSPECTION RH SIDE

DO A ROTOTEST

INSPECTION LH SIDE

INSTALL THE FASTENERS

RH SIDE

INSTALL THE FASTENERS

LH SIDE

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

11.50

5.75

STEPS

2.00 1.00

0

1.00 1.00

1.00 1.00

1.50 1.50

1.50 1.50

1.00 1.00

2.50 1.25

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

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

1

1

1

1

1

2

1.00 1.00 1

:

:

SB ELAPSED TIME

(HOURS)

1

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

2 3 4 5 6

D_SB_576115_5_ABAA_01_01

Figure A-FABAA - Sheet 01

Gantt Chart for Rototest Inspection

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 3

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Appendix 01: Elapsed Time Assumption

**CONF 002 thru 003

GET ACCESS

REMOVE

REMOVE 

DO A ROTOTEST

DO A ROTOTEST 

INSTALL 

INSTALL 

CLOSE−UP

THE FASTENERS 

RH SIDE

THE FASTENERS 

LH SIDE

INSPECTION RH SIDE

INSPECTION LH SIDE

THE FASTENERS 

RH SIDE

THE FASTENERS 

LH SIDE

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

43.00

21.50

STEPS

12.00 6.00

0

1.00 1.00

1.00 1.00

1.50 1.50

1.50 1.50

1.00 1.00

PER

2

1

1

1

1

1

1.00 1.00 1

24.00 12.00 2

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−57−6115

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:

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

MH ARE NOT REFLECTED IN THIS GANTT CHART.

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

: NUMBER OF PERSONS

:

5 10 15 20 25 30

SB ELAPSED TIME

(HOURS)

D_SB_576115_5_ABAB_01_00

Figure A-FABAB - Sheet 01

Gantt Chart for Rototest Inspection

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 Page: 4

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SERVICE BULLETIN

REPORTING SHEET

TITLE: WINGS-STRUCTURE-INSPECTION OF FR40 LOWER JUNCTION

FASTENER HOLES

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: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

REVISION No.: 00 - Apr 04/14 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: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115

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