# @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. 

# MANDATORYMANDATORYMANDATORY
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 fittingaround 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 5

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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 5

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# @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 5

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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

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# @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



# MANDATORYMANDATORYMANDATORY
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 5

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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 REVISION No.: 00 - Apr 04/14 Page: 2 5

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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 5

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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 5

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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 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 5

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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 intolerance 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 Before next flight None No cracks found

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 5

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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 intolerance 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 Before next flight None No cracks found

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 5

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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 intolerance 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 Before next flight None No cracks found

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 5

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# @A300-600 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 intolerance 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 Before next flight None No cracks found

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 5

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# @A300-600 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 intolerance 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 Before next flight None No cracks found

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: 11 5

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# @A300-600 SERVICE BULLETIN
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 intolerance 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 Before next flight None No cracks found

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 REVISION No.: 00 - Apr 04/14 Page: 12 5

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# @A300-600 SERVICE BULLETIN
**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 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 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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 14 5

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# @A300-600 SERVICE BULLETIN
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
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# @A300-600 SERVICE BULLETIN
M. SPARES None

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 16 5

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# @A300-600 SERVICE BULLETIN
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

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# @A300-600 SERVICE BULLETIN
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.
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# @A300-600 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

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# @A300-600 SERVICE BULLETIN

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# @A300-600 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.
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# @A300-600 SERVICE BULLETIN
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 DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 22 5

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# @A300-600 SERVICE BULLETIN (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.

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# @A300-600 SERVICE BULLETIN
**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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# @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 576115-941-001-001 - 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 REVISION No.: 00 - Apr 04/14 Page: 25 5

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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 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 REVISION No.: 00 - Apr 04/14 Page: 26 5

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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 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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# @A300-600 SERVICE BULLETIN
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. DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 28 5

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# @A300-600 SERVICE BULLETIN (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
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# @A300-600 SERVICE BULLETIN

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 REVISION No.: 00 - Apr 04/14 Page: 30 5

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# @A300-600 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 REVISION No.: 00 - Apr 04/14 Page: 31 5

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# @A300-600 SERVICE BULLETIN

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 REVISION No.: 00 - Apr 04/14 Page: 32 5

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# @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 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 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 00 - Apr 04/14 Page: 34 5

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# @A300-600 SERVICE BULLETIN

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 REVISION No.: 00 - Apr 04/14 Page: 35 5

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# @A300-600 SERVICE BULLETIN
**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 5

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# @A300-600 SERVICE BULLETIN
**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 REVISION No.: 00 - Apr 04/14 Page: 37 5

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# @A300-600 SERVICE BULLETIN (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: 38 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 **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 REVISION No.: 00 - Apr 04/14 Page: 39 5

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# @A300-600 SERVICE BULLETIN 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

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 40 5

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# @A300-600 SERVICE BULLETIN
**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 REVISION No.: 00 - Apr 04/14 Page: 41 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 00 - Apr 04/14 Page: 42 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 00 - Apr 04/14 Page: 43 5

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# @A300-600 SERVICE BULLETIN (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 5

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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

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# @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 5

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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 5

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# @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

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# @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

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# @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 5

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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 5

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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 5

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# @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

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# @A300-600 SERVICE BULLETIN
Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON 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 5

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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

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# @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

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# @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 5

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 5

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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 5

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# @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 5

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# @A300-600 SERVICE BULLETIN

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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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

# @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 5

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

# @A300-600 SERVICE BULLETIN (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 5

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

# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN
<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 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 SERVICE BULLETIN

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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# @A300-600 SERVICE BULLETIN

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 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN (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 5

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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 5

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# @A300-600 SERVICE BULLETIN

**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 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL



## B **B**

INSPECTION AREA **NOTE:** 

### B

**B** INBOARD SIDE WING 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 5

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# @A300-600 SERVICE BULLETIN

**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 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

FASTENERS HOLES

TO BE INSPECTED RIB1

WING SIDE INBOARD SIDE 01

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

## 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN

**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 5

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# @A300-600 SERVICE BULLETIN

**CONF 001

APPLY POLYSULFIDE SEALANT MAT. No 06ABA1 **NOTE:** 01 

## A **A** 1 2 (1) (2)

(3) (4)3 4 INBOARD SIDE WING SIDE 01 02

01 02

PROTECT THE FASTENERS HEADS AND NUTS WITH PRIMER POLYURETHANE PAINT 02 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 5

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# @A300-600 SERVICE BULLETIN

**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 5

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# @A300-600 SERVICE BULLETIN

**CONF 002



## A **A** 1 2 (1) (2)

(3) (4)3 4 INBOARD SIDE WING SIDE 01 02

01 02

APPLY POLYSULFIDE SEALANT MAT. No 06ABA1 **NOTE:** 01 PROTECT THE FASTENERS HEADS AND NUTS WITH PRIMER POLYURETHANE PAINT 02 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 5

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# @A300-600 SERVICE BULLETIN

**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 5

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# @A300-600 SERVICE BULLETIN

**CONF 003



## A **A** 1 2 (1) (2)

(3) (4)3 4 INBOARD SIDE WING SIDE 01 02

01 02

APPLY POLYSULFIDE SEALANT MAT. No 06ABA1 **NOTE:** 01 PROTECT THE FASTENERS HEADS AND NUTS WITH PRIMER POLYURETHANE PAINT 02 MAT. No 04EAC2 AND TOP COAT POLYURETHANE MAT. No 04JME4

HOLE SYMBOL DESCRIPTION BOLT NUT BOLT NUT F (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 5

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# @A300-600 SERVICE BULLETIN

**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, FR40LOWER 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 5

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# @A300-600 SERVICE BULLETIN

**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 5

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# @A300-600 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 92 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN 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

3 0 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 SERVICE BULLETIN 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 ARE NOT REFLECTED IN THIS GANTT CHART. MH 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 5

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# @A300-600 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 5

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

# @A300-600 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Apr 04/14 SERVICE BULLETIN No.: A300-57-6115 REVISION No.: 00 - Apr 04/14 Page: 1 5

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