# Airbus Service Bulletin A300-53-6176

Copy: No revision named ("SB A300-53-6176(2)"), 751 pages: PDF https://openairdocs.org/files/sha256/6e/08/6e08f0f5b246d48e8051e4e172c2d455ffef48dbe2bb62b9f7486923349ae9fc; text https://openairdocs.org/service-documents/airbus/a300-53-6176/file/6e08f0f5b246.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2014-0143; AD 2016-25-27 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A300-53-6176
- Page: https://openairdocs.org/service-documents/airbus/a300-53-6176

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2016-25-27](https://openairdocs.org/ad/2016-25-27.md), effective Feb 8, 2017: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a300-53-6176/proposed.md).

## Text (751 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2014-0143; AD 2016-25-27 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A300-600
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 53
TITLE: FUSELAGE - CENTER SECTION - REPLACE ALL LOWER FRAME FEET
FROM FR41 TO FR46
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 13721S22901
MINOR
 None
NOTE
: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
Due to In Service Occurrence and Widespread Fatigue Damage (WFD) analysis result, it is
recommended to improve the lower frame feet design from Frame 41 to Frame 46.
The modification consists in replacing lower frame feet from Frame 41 to Frame 46 by optimized parts
and installation. Accomplishment of modification Service Bulletin (SB) No. A300-53-6176 cancels the
requirements of the Inspection Service Bulletin (ISB) No. A300-53-6177.
Accomplishment of this Service Bulletin will increase the service life of junctions of center box lower
frame bases from frame Frame 41 to Frame 46.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 RECOMMENDED (1)
 CANCELS INSPECTION SB
 YES
POTENTIAL AD
 NO
 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
DE-FUELLING/VENTILATION
 YES
NOTE
 (1)
: Service Bulletin recommended to be accomplished to prevent significant operational
disruptions.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@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
Kit 536176A01R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A04R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A07R01
 1
 12,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A10R01
 1
 12,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A13R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A16R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A19R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A22R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A25R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A28R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A31R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A34R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
TOTAL
 133,500.00
Component COMPA01
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA02
 4
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA03
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA04
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA05
 2
 See SB
 B o l t ,N u t ,R i v e t
**CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 536176A02R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A05R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A08R01
 1
 12,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A11R01
 1
 12,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A14R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A17R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A20R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A23R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A26R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A29R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A32R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A35R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A300-600
SERVICE BULLETIN
SUMMARY
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
TOTAL
 132,500.00
Component COMPA01
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA02
 4
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA03
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA04
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA05
 2
 See SB
 B o l t ,N u t ,R i v e t
**CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 536176A03R01
 1
 11,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A06R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A09R01
 1
 11,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A12R01
 1
 11,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A15R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A18R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A21R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A24R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A27R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A30R01
 1
 10,500.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A33R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
Kit 536176A36R01
 1
 11,000.00
 Frame foot, Splice, Bolt, Nut, Rivet
TOTAL
 131,500.00
Component COMPA01
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA02
 4
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA03
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA04
 2
 See SB
 B o l t ,N u t ,R i v e t
Component COMPA05
 2
 See SB
 B o l t ,N u t ,R i v e t
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
06P 67Q ABR AHK BCS F2I FDX IRA IRM KAC MNB MRJ MSR
OHY SUD TAR THA UPS UQA URS UTP UZB
CONCURRENT REQUIREMENTS
None
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A300-600
SERVICE BULLETIN
SUMMARY
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
SOFT
 NO
OBRM
 NO
MANPOWER
**CONF 001
Task 536176-831-801-001: Modification
TOTAL MANHOURS
 529.00
ELAPSED TIME (HOURS)
 69.00
**CONF 002
Task 536176-831-801-001: Modification
TOTAL MANHOURS
 529.00
ELAPSED TIME (HOURS)
 69.00
**CONF 003
Task 536176-831-801-001: Modification
TOTAL MANHOURS
 529.00
ELAPSED TIME (HOURS)
 69.00
APPENDICES
**CONF ALL
Appendix 01 - Elapsed Time Assumption
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A300-600
SERVICE BULLETIN
SUMMARY
**CONF ALL
FR41
FR42
FR43
FR44
FR45
FR46
FR47
FR40
FR46
FR45
FR44
FR43
FR42
FR41
CL
A
B
Z140
A
FRAME FEET
TO BE MODIFIED
B
D_SB_536176_5_SAAA_01_01
Figure A-FSAAA - Sheet 01
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A300-600
SERVICE BULLETIN
SUMMARY
This Page Intentionally Left Blank
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A300-600
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
ATA SYSTEM: 53
TITLE: FUSELAGE - CENTER SECTION - REPLACE ALL LOWER FRAME FEET
FROM FR41 TO FR46
MODIFICATION No.: 13721S22901
This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the
property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with
any information contained in it. It is delivered on the express condition that said document and the
information contained in it shall be treated as confidential, shall not be used for any purpose other than
that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall
not be duplicated in any manner (except for the purposes of performing the tasks described hereunder
and provided that any recipient of such document shall comply with the conditions herein), without
AIRBUS prior written consent.
1. PLANNING INFORMATION
**CONF ALL
A. EFFECTIVITY
NOTE
: This modification is applicable by Service Bulletin only.
(1) Models
B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/F C4-620 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 0579 0581 0584 0602-0603 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 0683 0688 0694 0696 0699 0701 0703 0707 0709 0711 0713 0715
0717 0719 0721-0730 0732-0750 0752-0764 0766 0768-0775 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: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A300-600
SERVICE BULLETIN
OPERATOR
 MSN
06P
 0788
67Q
 0584 0603 0744 0749 0764
ABR
 0677 0743
AHK
 0683 0770 0855 0856 0857 0858 0859 0860 0870 0871
BCS
 0529 0557 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724
0729 0730 0737 0740 0753 0783 0797 0836 0837 0872
F2I
 0294
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
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
MNB
 0521 0525 0532 0734 0739 0755 0756 0758
MRJ
 0750 0762
MSR
 0561 0607
OHY
 0747
SUD
 0666 0775
TAR
 0505 0558 0563
THA
 0629 0782 0784 0785 0786 0787
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
UQA
 0626 0643
URS
 0733
UTP
 0707 0725 0732 0741 0746 0754 0763
UZB
 0717 0722
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A300-600
SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
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 0558 0559 0561 0563 0572 0575
0579 0581 0584 0602 0603 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 0683 0688
0694 0696 0699 0701 0703 0707 0709 0711 0713 0715 0717
0719 0721 0722 0723 0724 0725 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 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
001 002 003
0747
 001
(5) Configuration definition
NOTE
: Each frame foot is independent, the operator must define which repair
has been applied or not on each frame foot and choose the configuration
that applies for each frame foot.
**CONF 001
Config. 001 is valid for aircraft on which the frame foot have been repaired in
accordance with Repair Drawing R53810322 and/or R53810323 and/or R53810329
and/or R53810330 and/or R53810331 and/or R53810332.
**CONF 002
Config. 002 is valid for aircraft on which the frame foot have been repaired in
accordance with Service Bulletin (SB) No. A300-53-6111.
**CONF 003
Config. 003 is valid for aircraft on which the frame foot have not been repaired.
(6) Material Effectivity
**CONF 001
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 536176A01R01
 1
Kit 536176A04R01
 1
Kit 536176A07R01
 1
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A300-600
SERVICE BULLETIN
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 536176A10R01
 1
Kit 536176A13R01
 1
Kit 536176A16R01
 1
Kit 536176A19R01
 1
Kit 536176A22R01
 1
Kit 536176A25R01
 1
Kit 536176A28R01
 1
Kit 536176A31R01
 1
Kit 536176A34R01
 1
Component COMPA01
 2
Component COMPA02
 4
Component COMPA03
 2
Component COMPA04
 2
Component COMPA05
 2
Consumable CMLA01
 1
**CONF 002
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 536176A02R01
 1
Kit 536176A05R01
 1
Kit 536176A08R01
 1
Kit 536176A11R01
 1
Kit 536176A14R01
 1
Kit 536176A17R01
 1
Kit 536176A20R01
 1
Kit 536176A23R01
 1
Kit 536176A26R01
 1
Kit 536176A29R01
 1
Kit 536176A32R01
 1
Kit 536176A35R01
 1
Component COMPA01
 2
Component COMPA02
 4
Component COMPA03
 2
Component COMPA04
 2
Component COMPA05
 2
Consumable CMLA01
 1
**CONF 003
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 536176A03R01
 1
Kit 536176A06R01
 1
Kit 536176A09R01
 1
Kit 536176A12R01
 1
Kit 536176A15R01
 1
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A300-600
SERVICE BULLETIN
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 536176A18R01
 1
Kit 536176A21R01
 1
Kit 536176A24R01
 1
Kit 536176A27R01
 1
Kit 536176A30R01
 1
Kit 536176A33R01
 1
Kit 536176A36R01
 1
Component COMPA01
 2
Component COMPA02
 4
Component COMPA03
 2
Component COMPA04
 2
Component COMPA05
 2
Consumable CMLA01
 1
**CONF ALL
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
Due to In Service Occurrence and Widespread Fatigue Damage (WFD) analysis result, it
is recommended to improve the lower frame feet design from Frame 41 to Frame 46.
(2) Objective/Action
The modification consists in replacing lower frame feet from Frame 41 to Frame 46 by
optimized parts and installation. Accomplishment of modification Service Bulletin (SB)
No. A300-53-6176 cancels the requirements of the Inspection Service Bulletin (ISB) No.
A300-53-6177.
(3) Advantages
Accomplishment of this Service Bulletin will increase the service life of junctions of
center box lower frame bases from frame Frame 41 to Frame 46.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A300-600
SERVICE BULLETIN
**CONF 001
Task 536176-831-801-001: Modification
(1) If Necessary, Remove Fasteners from FR41, LH side
(2) Remove the gussets from FR41, LH side
(3) Remove the Frame Foot from FR41, LH side
(4) Install the Optimized Frame Foot at FR41, LH side
(5) On bench, install the Nuts on the Gussets of the Frame Foot FR41, LH side
(6) If Removed, Install the Fasteners at FR41, LH side
(7) If Necessary, Remove Fasteners from FR41, RH side
(8) Remove the gussets from FR41, RH side
(9) Remove the Frame Foot from FR41, RH side
(10) Install the Optimized Frame Foot at FR41, RH side
(11) On bench, install the Nuts on the Gussets of the Frame Foot FR41, RH side
(12) If Removed, Install the Fasteners at FR41, RH side
(13) If necessary, Remove Fasteners from FR42 LH side
(14) Remove the Gusset from FR42, LH side
(15) Remove the Frame Foot from FR42, LH side
(16) Install the Optimized Frame Foot at FR42, LH side
(17) On bench, install the Nuts on the Gussets of the Frame Foot FR42, LH side
(18) If removed, Install the Fasteners at FR42 LH side
(19) If necessary, Remove Fasteners from FR 42, RH side
(20) Remove the Gussets from FR42, RH side
(21) Remove the Frame Foot from FR42, RH side
(22) Install the Optimized Frame Foot at FR42, RH side
(23) On bench, install the Nuts on the Gussets of the Frame Foot FR42, RH side
(24) If removed, Install the Fasteners at FR42, RH side
(25) If necessary, Remove Fasteners from FR43, LH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 13

@A300-600
SERVICE BULLETIN
(26) Remove the Gussets from FR43, LH side
(27) Remove the Frame Foot from FR43, LH side
(28) Install the Optimized Frame Foot at FR43, LH side
(29) On bench, install the Nuts on the Gussets of the Frame Foot FR43, LH side
(30) If removed, Install the Fasteners at FR43, LH side
(31) If necessary, Remove Fasteners from FR43, RH side
(32) Remove the Gussets from FR43, RH side
(33) Remove the Frame Foot from FR43, RH side
(34) Install the Optimized Frame Foot at FR43, RH side
(35) On bench, install the Nuts on the Gussets of the Frame Foot FR43, RH side
(36) If removed, Install the Fasteners at FR43, RH side
(37) If necessary, Remove Fasteners from FR44, LH side
(38) Remove the Gussets from FR44, LH side
(39) Remove the Frame Foot from FR44, LH side
(40) Install the Optimized Frame Foot at FR44, LH side
(41) On bench, install the Nuts on the Gussets of the Frame Foot FR44, LH side
(42) If removed, Install the Fasteners at FR44, LH side
(43) If necessary, Remove Fasteners from FR44, RH side
(44) Remove the Gussets from FR44, RH side
(45) Remove the Frame Foot from FR44, RH side
(46) Install the Optimized Frame Foot at FR44, RH side
(47) On bench, install the Nuts on the Gussets of the Frame Foot FR44, RH side
(48) If removed, Install the Fasteners at FR44, RH side
(49) If necessary, Remove Fasteners from FR45, LH side
(50) Remove the Gussets from FR45, LH side
(51) Remove the Frame Foot from FR45, LH side
(52) Install the Optimized Frame Foot at FR45, LH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 7
5
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### Page 14

@A300-600
SERVICE BULLETIN
(53) On bench, install the Nuts on the Gussets of the Frame Foot FR45, LH side
(54) If removed, Install the Fasteners at FR45, LH side
(55) If necessary, Remove Fasteners from FR45, RH side
(56) Remove the Gussets from FR45, RH side
(57) Remove the Frame Foot from FR45, RH side
(58) Install the Optimized Frame Foot at FR45, RH side
(59) On bench, install the Nuts on the Gussets of the Frame Foot FR45, RH side
(60) If removed, Install the Fasteners at FR45, RH side
(61) If necessary, Remove Fasteners from FR46, LH side
(62) Remove the Gussets from FR46, LH side
(63) Remove the Frame Foot from FR46, LH side
(64) Install the Optimized Frame Foot at FR46, LH side
(65) On bench, install the Nuts on the Gussets of the Frame Foot FR46, LH side
(66) If removed, Install the Fasteners at FR46, LH side
(67) If necessary, Remove Fasteners from FR46, RH side
(68) Remove the Gussets from FR46, RH side
(69) Remove the Frame Foot from FR46, RH side
(70) Install the Optimized Frame Foot at FR46, RH side
(71) On bench, install the Nuts on the Gussets of the Frame Foot FR46, RH side
(72) If removed, Install the Fasteners at FR46, RH side
**CONF 002
Task 536176-831-801-001: Modification
(1) If Necessary, Remove Fasteners from FR41, LH side
(2) Remove the gussets from FR41, LH side
(3) Remove the Frame Foot from FR41, LH side
(4) Install the Optimized Frame Foot at FR41, LH side
(5) On bench, install the Nuts on the Gussets of the Frame Foot FR41, LH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 8
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 15

@A300-600
SERVICE BULLETIN
(6) If Removed, Install the Fasteners at FR41, LH side
(7) If Necessary, Remove Fasteners from FR41, RH side
(8) Remove the gussets from FR41, RH side
(9) Remove the Frame Foot from FR41, RH side
(10) Install the Optimized Frame Foot at FR41, RH side
(11) On bench, install the Nuts on the Gussets of the Frame Foot FR41, RH side
(12) If Removed, Install the Fasteners at FR41, RH side
(13) If necessary, Remove Fasteners from FR42 LH side
(14) Remove the Gusset from FR42, LH side
(15) Remove the Frame Foot from FR42, LH side
(16) Install the Optimized Frame Foot at FR42, LH side
(17) On bench, install the Nuts on the Gussets of the Frame Foot FR42, LH side
(18) If removed, Install the Fasteners at FR42 LH side
(19) If necessary, Remove Fasteners from FR 42, RH side
(20) Remove the Gussets from FR42, RH side
(21) Remove the Frame Foot from FR42, RH side
(22) Install the Optimized Frame Foot at FR42, RH side
(23) On bench, install the Nuts on the Gussets of the Frame Foot FR42, RH side
(24) If removed, Install the Fasteners at FR42, RH side
(25) If necessary, Remove Fasteners from FR43, LH side
(26) Remove the Gussets from FR43, LH side
(27) Remove the Frame Foot from FR43, LH side
(28) Install the Optimized Frame Foot at FR43, LH side
(29) On bench, install the Nuts on the Gussets of the Frame Foot FR43, LH side
(30) If removed, Install the Fasteners at FR43, LH side
(31) If necessary, Remove Fasteners from FR43, RH side
(32) Remove the Gussets from FR43, RH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 9
5
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### Page 16

@A300-600
SERVICE BULLETIN
(33) Remove the Frame Foot from FR43, RH side
(34) Install the Optimized Frame Foot at FR43, RH side
(35) On bench, install the Nuts on the Gussets of the Frame Foot FR43, RH side
(36) If removed, Install the Fasteners at FR43, RH side
(37) If necessary, Remove Fasteners from FR44, LH side
(38) Remove the Gussets from FR44, LH side
(39) Remove the Frame Foot from FR44, LH side
(40) Install the Optimized Frame Foot at FR44, LH side
(41) On bench, install the Nuts on the Gussets of the Frame Foot FR44, LH side
(42) If removed, Install the Fasteners at FR44, LH side
(43) If necessary, Remove Fasteners from FR44, RH side
(44) Remove the Gussets from FR44, RH side
(45) Remove the Frame Foot from FR44, RH side
(46) Install the Optimized Frame Foot at FR44, RH side
(47) On bench, install the Nuts on the Gussets of the Frame Foot FR44, RH side
(48) If removed, Install the Fasteners at FR44, RH side
(49) If necessary, Remove Fasteners from FR45, LH side
(50) Remove the Gussets from FR45, LH side
(51) Remove the Frame Foot from FR45, LH side
(52) Install the Optimized Frame Foot at FR45, LH side
(53) On bench, install the Nuts on the Gussets of the Frame Foot FR45, LH side
(54) If removed, Install the Fasteners at FR45, LH side
(55) If necessary, Remove Fasteners from FR45, RH side
(56) Remove the Gussets from FR45, RH side
(57) Remove the Frame Foot from FR45, RH side
(58) Install the Optimized Frame Foot at FR45, RH side
(59) On bench, install the Nuts on the Gussets of the Frame Foot FR45, RH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 10
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 17

@A300-600
SERVICE BULLETIN
(60) If removed, Install the Fasteners at FR45, RH side
(61) If necessary, Remove Fasteners from FR46, LH side
(62) Remove the Gussets from FR46, LH side
(63) Remove the Frame Foot from FR46, LH side
(64) Install the Optimized Frame Foot at FR46, LH side
(65) On bench, install the Nuts on the Gussets of the Frame Foot FR46, LH side
(66) If removed, Install the Fasteners at FR46, LH side
(67) If necessary, Remove Fasteners from FR46, RH side
(68) Remove the Gussets from FR46, RH side
(69) Remove the Frame Foot from FR46, RH side
(70) Install the Optimized Frame Foot at FR46, RH side
(71) On bench, install the Nuts on the Gussets of the Frame Foot FR46, RH side
(72) If removed, Install the Fasteners at FR46, RH side
**CONF 003
Task 536176-831-801-001: Modification
(1) If Necessary, Remove Fasteners from FR41, LH side
(2) Remove the gussets from FR41, LH side
(3) Remove the Frame Foot from FR41, LH side
(4) Install the Optimized Frame Foot at FR41, LH side
(5) On bench, install the Nuts on the Gussets of the Frame Foot FR41, LH side
(6) If Removed, Install the Fasteners at FR41, LH side
(7) If Necessary, Remove Fasteners from FR41, RH side
(8) Remove the gussets from FR41, RH side
(9) Remove the Frame Foot from FR41, RH side
(10) Install the Optimized Frame Foot at FR41, RH side
(11) On bench, install the Nuts on the Gussets of the Frame Foot FR41, RH side
(12) If Removed, Install the Fasteners at FR41, RH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 11
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 18

@A300-600
SERVICE BULLETIN
(13) If necessary, Remove Fasteners from FR42 LH side
(14) Remove the Gusset from FR42, LH side
(15) Remove the Frame Foot from FR42, LH side
(16) Install the Optimized Frame Foot at FR42, LH side
(17) On bench, install the Nuts on the Gussets of the Frame Foot FR42, LH side
(18) If removed, Install the Fasteners at FR42 LH side
(19) If necessary, Remove Fasteners from FR 42, RH side
(20) Remove the Gussets from FR42, RH side
(21) Remove the Frame Foot from FR42, RH side
(22) Install the Optimized Frame Foot at FR42, RH side
(23) On bench, install the Nuts on the Gussets of the Frame Foot FR42, RH side
(24) If removed, Install the Fasteners at FR42, RH side
(25) If necessary, Remove Fasteners from FR43, LH side
(26) Remove the Gussets from FR43, LH side
(27) Remove the Frame Foot from FR43, LH side
(28) Install the Optimized Frame Foot at FR43, LH side
(29) On bench, install the Nuts on the Gussets of the Frame Foot FR43, LH side
(30) If removed, Install the Fasteners at FR43, LH side
(31) If necessary, Remove Fasteners from FR43, RH side
(32) Remove the Gussets from FR43, RH side
(33) Remove the Frame Foot from FR43, RH side
(34) Install the Optimized Frame Foot at FR43, RH side
(35) On bench, install the Nuts on the Gussets of the Frame Foot FR43, RH side
(36) If removed, Install the Fasteners at FR43, RH side
(37) If necessary, Remove Fasteners from FR44, LH side
(38) Remove the Gussets from FR44, LH side
(39) Remove the Frame Foot from FR44, LH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 12
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 19

@A300-600
SERVICE BULLETIN
(40) Install the Optimized Frame Foot at FR44, LH side
(41) On bench, install the Nuts on the Gussets of the Frame Foot FR44, LH side
(42) If removed, Install the Fasteners at FR44, LH side
(43) If necessary, Remove Fasteners from FR44, RH side
(44) Remove the Gussets from FR44, RH side
(45) Remove the Frame Foot from FR44, RH side
(46) Install the Optimized Frame Foot at FR44, RH side
(47) On bench, install the Nuts on the Gussets of the Frame Foot FR44, RH side
(48) If removed, Install the Fasteners at FR44, RH side
(49) If necessary, Remove Fasteners from FR45, LH side
(50) Remove the Gussets from FR45, LH side
(51) Remove the Frame Foot from FR45, LH side
(52) Install the Optimized Frame Foot at FR45, LH side
(53) On bench, install the Nuts on the Gussets of the Frame Foot FR45, LH side
(54) If removed, Install the Fasteners at FR45, LH side
(55) If necessary, Remove Fasteners from FR45, RH side
(56) Remove the Gussets from FR45, RH side
(57) Remove the Frame Foot from FR45, RH side
(58) Install the Optimized Frame Foot at FR45, RH side
(59) On bench, install the Nuts on the Gussets of the Frame Foot FR45, RH side
(60) If removed, Install the Fasteners at FR45, RH side
(61) If necessary, Remove Fasteners from FR46, LH side
(62) Remove the Gussets from FR46, LH side
(63) Remove the Frame Foot from FR46, LH side
(64) Install the Optimized Frame Foot at FR46, LH side
(65) On bench, install the Nuts on the Gussets of the Frame Foot FR46, LH side
(66) If removed, Install the Fasteners at FR46, LH side
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 13
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 20

@A300-600
SERVICE BULLETIN
(67) If necessary, Remove Fasteners from FR46, RH side
(68) Remove the Gussets from FR46, RH side
(69) Remove the Frame Foot from FR46, RH side
(70) Install the Optimized Frame Foot at FR46, RH side
(71) On bench, install the Nuts on the Gussets of the Frame Foot FR46, RH side
(72) If removed, Install the Fasteners at FR46, RH side
**CONF ALL
E. COMPLIANCE
(1) Classification
RECOMMENDED: Service Bulletin recommended to be accomplished to prevent
significant operational disruptions.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin is recommended at the earliest opportunity
where manpower and facilities are available.
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.
**CONF 001
Task 536176-831-801-001: Modification
Get Access
 3.00
On Aircraft
If Necessary, Remove Fasteners from FR41, LH side
 4.00
Remove the gussets from FR41, LH side
 1.00
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 14
5
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### Page 21

@A300-600
SERVICE BULLETIN
Task 536176-831-801-001: Modification
Remove the Frame Foot from FR41, LH side
 16.00
Install the Optimized Frame Foot at FR41, LH side
 16.00
If Removed, Install the Fasteners at FR41, LH side
 6.00
If Necessary, Remove Fasteners from FR41, RH side
 4.00
Remove the gussets from FR41, RH side
 1.00
Remove the Frame Foot from FR41, RH side
 16.00
Install the Optimized Frame Foot at FR41, RH side
 16.00
If Removed, Install the Fasteners at FR41, RH side
 6.00
If necessary, Remove Fasteners from FR42 LH side
 4.00
Remove the Gusset from FR42, LH side
 1.00
Remove the Frame Foot from FR42, LH side
 16.00
Install the Optimized Frame Foot at FR42, LH side
 16.00
If removed, Install the Fasteners at FR42 LH side
 6.00
If necessary, Remove Fasteners from FR 42, RH side
 4.00
Remove the Gussets from FR42, RH side
 1.00
Remove the Frame Foot from FR42, RH side
 16.00
Install the Optimized Frame Foot at FR42, RH side
 16.00
If removed, Install the Fasteners at FR42, RH side
 6.00
If necessary, Remove Fasteners from FR43, LH side
 4.00
Remove the Gussets from FR43, LH side
 1.00
Remove the Frame Foot from FR43, LH side
 16.00
Install the Optimized Frame Foot at FR43, LH side
 16.00
If removed, Install the Fasteners at FR43, LH side
 6.00
If necessary, Remove Fasteners from FR43, RH side
 4.00
Remove the Gussets from FR43, RH side
 1.00
Remove the Frame Foot from FR43, RH side
 16.00
Install the Optimized Frame Foot at FR43, RH side
 16.00
If removed, Install the Fasteners at FR43, RH side
 6.00
If necessary, Remove Fasteners from FR44, LH side
 4.00
Remove the Gussets from FR44, LH side
 1.00
Remove the Frame Foot from FR44, LH side
 16.00
Install the Optimized Frame Foot at FR44, LH side
 16.00
If removed, Install the Fasteners at FR44, LH side
 6.00
If necessary, Remove Fasteners from FR44, RH side
 4.00
Remove the Gussets from FR44, RH side
 1.00
Remove the Frame Foot from FR44, RH side
 16.00
Install the Optimized Frame Foot at FR44, RH side
 16.00
If removed, Install the Fasteners at FR44, RH side
 6.00
If necessary, Remove Fasteners from FR45, LH side
 4.00
Remove the Gussets from FR45, LH side
 1.00
Remove the Frame Foot from FR45, LH side
 16.00
Install the Optimized Frame Foot at FR45, LH side
 16.00
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 15
5
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### Page 22

@A300-600
SERVICE BULLETIN
Task 536176-831-801-001: Modification
If removed, Install the Fasteners at FR45, LH side
 6.00
If necessary, Remove Fasteners from FR45, RH side
 4.00
Remove the Gussets from FR45, RH side
 1.00
Remove the Frame Foot from FR45, RH side
 16.00
Install the Optimized Frame Foot at FR45, RH side
 16.00
If removed, Install the Fasteners at FR45, RH side
 6.00
If necessary, Remove Fasteners from FR46, LH side
 4.00
Remove the Gussets from FR46, LH side
 1.00
Remove the Frame Foot from FR46, LH side
 16.00
Install the Optimized Frame Foot at FR46, LH side
 16.00
If removed, Install the Fasteners at FR46, LH side
 6.00
If necessary, Remove Fasteners from FR46, RH side
 4.00
Remove the Gussets from FR46, RH side
 1.00
Remove the Frame Foot from FR46, RH side
 16.00
Install the Optimized Frame Foot at FR46, RH side
 16.00
If removed, Install the Fasteners at FR46, RH side
 6.00
On Bench
On bench, install the Nuts on the Gussets of the
Frame Foot FR41, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR41, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR42, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR42, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR43, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR43, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR44, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR44, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR45, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR45, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR46, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR46, RH side
0.50
Close-Up
 4.00
TOTAL MANHOURS
 529.00
ELAPSED TIME (HOURS)
 69.00
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 16
5
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### Page 23

@A300-600
SERVICE BULLETIN
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAAAA
 given in Appendix 01 - Elapsed Time Assumption .
**CONF 002
Task 536176-831-801-001: Modification
Get Access
 3.00
On Aircraft
If Necessary, Remove Fasteners from FR41, LH side
 4.00
Remove the gussets from FR41, LH side
 1.00
Remove the Frame Foot from FR41, LH side
 16.00
Install the Optimized Frame Foot at FR41, LH side
 16.00
If Removed, Install the Fasteners at FR41, LH side
 6.00
If Necessary, Remove Fasteners from FR41, RH side
 4.00
Remove the gussets from FR41, RH side
 1.00
Remove the Frame Foot from FR41, RH side
 16.00
Install the Optimized Frame Foot at FR41, RH side
 16.00
If Removed, Install the Fasteners at FR41, RH side
 6.00
If necessary, Remove Fasteners from FR42 LH side
 4.00
Remove the Gusset from FR42, LH side
 1.00
Remove the Frame Foot from FR42, LH side
 16.00
Install the Optimized Frame Foot at FR42, LH side
 16.00
If removed, Install the Fasteners at FR42 LH side
 6.00
If necessary, Remove Fasteners from FR 42, RH side
 4.00
Remove the Gussets from FR42, RH side
 1.00
Remove the Frame Foot from FR42, RH side
 16.00
Install the Optimized Frame Foot at FR42, RH side
 16.00
If removed, Install the Fasteners at FR42, RH side
 6.00
If necessary, Remove Fasteners from FR43, LH side
 4.00
Remove the Gussets from FR43, LH side
 1.00
Remove the Frame Foot from FR43, LH side
 16.00
Install the Optimized Frame Foot at FR43, LH side
 16.00
If removed, Install the Fasteners at FR43, LH side
 6.00
If necessary, Remove Fasteners from FR43, RH side
 4.00
Remove the Gussets from FR43, RH side
 1.00
Remove the Frame Foot from FR43, RH side
 16.00
Install the Optimized Frame Foot at FR43, RH side
 16.00
If removed, Install the Fasteners at FR43, RH side
 6.00
If necessary, Remove Fasteners from FR44, LH side
 4.00
Remove the Gussets from FR44, LH side
 1.00
Remove the Frame Foot from FR44, LH side
 16.00
Install the Optimized Frame Foot at FR44, LH side
 16.00
If removed, Install the Fasteners at FR44, LH side
 6.00
If necessary, Remove Fasteners from FR44, RH side
 4.00
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 17
5
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### Page 24

@A300-600
SERVICE BULLETIN
Task 536176-831-801-001: Modification
Remove the Gussets from FR44, RH side
 1.00
Remove the Frame Foot from FR44, RH side
 16.00
Install the Optimized Frame Foot at FR44, RH side
 16.00
If removed, Install the Fasteners at FR44, RH side
 6.00
If necessary, Remove Fasteners from FR45, LH side
 4.00
Remove the Gussets from FR45, LH side
 1.00
Remove the Frame Foot from FR45, LH side
 16.00
Install the Optimized Frame Foot at FR45, LH side
 16.00
If removed, Install the Fasteners at FR45, LH side
 6.00
If necessary, Remove Fasteners from FR45, RH side
 4.00
Remove the Gussets from FR45, RH side
 1.00
Remove the Frame Foot from FR45, RH side
 16.00
Install the Optimized Frame Foot at FR45, RH side
 16.00
If removed, Install the Fasteners at FR45, RH side
 6.00
If necessary, Remove Fasteners from FR46, LH side
 4.00
Remove the Gussets from FR46, LH side
 1.00
Remove the Frame Foot from FR46, LH side
 16.00
Install the Optimized Frame Foot at FR46, LH side
 16.00
If removed, Install the Fasteners at FR46, LH side
 6.00
If necessary, Remove Fasteners from FR46, RH side
 4.00
Remove the Gussets from FR46, RH side
 1.00
Remove the Frame Foot from FR46, RH side
 16.00
Install the Optimized Frame Foot at FR46, RH side
 16.00
If removed, Install the Fasteners at FR46, RH side
 6.00
On Bench
On bench, install the Nuts on the Gussets of the
Frame Foot FR41, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR41, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR42, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR42, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR43, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR43, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR44, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR44, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR45, LH side
0.50
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 18
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 25

@A300-600
SERVICE BULLETIN
Task 536176-831-801-001: Modification
On bench, install the Nuts on the Gussets of the
Frame Foot FR45, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR46, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR46, RH side
0.50
Close-Up
 4.00
TOTAL MANHOURS
 529.00
ELAPSED TIME (HOURS)
 69.00
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAAAA
 given in Appendix 01 - Elapsed Time Assumption .
**CONF 003
Task 536176-831-801-001: Modification
Get Access
 3.00
On Aircraft
If Necessary, Remove Fasteners from FR41, LH side
 4.00
Remove the gussets from FR41, LH side
 1.00
Remove the Frame Foot from FR41, LH side
 16.00
Install the Optimized Frame Foot at FR41, LH side
 16.00
If Removed, Install the Fasteners at FR41, LH side
 6.00
If Necessary, Remove Fasteners from FR41, RH side
 4.00
Remove the gussets from FR41, RH side
 1.00
Remove the Frame Foot from FR41, RH side
 16.00
Install the Optimized Frame Foot at FR41, RH side
 16.00
If Removed, Install the Fasteners at FR41, RH side
 6.00
If necessary, Remove Fasteners from FR42 LH side
 4.00
Remove the Gusset from FR42, LH side
 1.00
Remove the Frame Foot from FR42, LH side
 16.00
Install the Optimized Frame Foot at FR42, LH side
 16.00
If removed, Install the Fasteners at FR42 LH side
 6.00
If necessary, Remove Fasteners from FR 42, RH side
 4.00
Remove the Gussets from FR42, RH side
 1.00
Remove the Frame Foot from FR42, RH side
 16.00
Install the Optimized Frame Foot at FR42, RH side
 16.00
If removed, Install the Fasteners at FR42, RH side
 6.00
If necessary, Remove Fasteners from FR43, LH side
 4.00
Remove the Gussets from FR43, LH side
 1.00
Remove the Frame Foot from FR43, LH side
 16.00
Install the Optimized Frame Foot at FR43, LH side
 16.00
If removed, Install the Fasteners at FR43, LH side
 6.00
If necessary, Remove Fasteners from FR43, RH side
 4.00
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 19
5
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### Page 26

@A300-600
SERVICE BULLETIN
Task 536176-831-801-001: Modification
Remove the Gussets from FR43, RH side
 1.00
Remove the Frame Foot from FR43, RH side
 16.00
Install the Optimized Frame Foot at FR43, RH side
 16.00
If removed, Install the Fasteners at FR43, RH side
 6.00
If necessary, Remove Fasteners from FR44, LH side
 4.00
Remove the Gussets from FR44, LH side
 1.00
Remove the Frame Foot from FR44, LH side
 16.00
Install the Optimized Frame Foot at FR44, LH side
 16.00
If removed, Install the Fasteners at FR44, LH side
 6.00
If necessary, Remove Fasteners from FR44, RH side
 4.00
Remove the Gussets from FR44, RH side
 1.00
Remove the Frame Foot from FR44, RH side
 16.00
Install the Optimized Frame Foot at FR44, RH side
 16.00
If removed, Install the Fasteners at FR44, RH side
 6.00
If necessary, Remove Fasteners from FR45, LH side
 4.00
Remove the Gussets from FR45, LH side
 1.00
Remove the Frame Foot from FR45, LH side
 16.00
Install the Optimized Frame Foot at FR45, LH side
 16.00
If removed, Install the Fasteners at FR45, LH side
 6.00
If necessary, Remove Fasteners from FR45, RH side
 4.00
Remove the Gussets from FR45, RH side
 1.00
Remove the Frame Foot from FR45, RH side
 16.00
Install the Optimized Frame Foot at FR45, RH side
 16.00
If removed, Install the Fasteners at FR45, RH side
 6.00
If necessary, Remove Fasteners from FR46, LH side
 4.00
Remove the Gussets from FR46, LH side
 1.00
Remove the Frame Foot from FR46, LH side
 16.00
Install the Optimized Frame Foot at FR46, LH side
 16.00
If removed, Install the Fasteners at FR46, LH side
 6.00
If necessary, Remove Fasteners from FR46, RH side
 4.00
Remove the Gussets from FR46, RH side
 1.00
Remove the Frame Foot from FR46, RH side
 16.00
Install the Optimized Frame Foot at FR46, RH side
 16.00
If removed, Install the Fasteners at FR46, RH side
 6.00
On Bench
On bench, install the Nuts on the Gussets of the
Frame Foot FR41, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR41, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR42, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR42, RH side
0.50
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 20
5
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### Page 27

@A300-600
SERVICE BULLETIN
Task 536176-831-801-001: Modification
On bench, install the Nuts on the Gussets of the
Frame Foot FR43, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR43, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR44, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR44, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR45, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR45, RH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR46, LH side
0.50
On bench, install the Nuts on the Gussets of the
Frame Foot FR46, RH side
0.50
Close-Up
 4.00
TOTAL MANHOURS
 529.00
ELAPSED TIME (HOURS)
 69.00
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAAAA
 given in Appendix 01 - Elapsed Time Assumption .
**CONF ALL
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Aircraft Maintenance Manual (AMM)
 06-21-00 06-31-53 06-41-00
06-41-53 20-21-12 20-28-11
24-00-00 28-00-00 28-10-00
28-11-29 28-13-21 28-25-00
32-12-11
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-51-20 20-55-00
Service Bulletin (SB)
 A300-53-6176
A300-53-6177
Standards Manual (SM)
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 21
5
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### Page 28

@A300-600
SERVICE BULLETIN
Structural Repair Manual (SRM)
 51-24-00 51-40-00 51-40-20
51-40-30 51-40-40 51-44-00
**CONF 002
Aircraft Maintenance Manual (AMM)
 06-21-00 06-31-53 06-41-00
06-41-53 20-21-12 20-28-11
24-00-00 28-00-00 28-10-00
28-11-29 28-13-21 28-25-00
32-12-11
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-51-20 20-55-00
Service Bulletin (SB)
 A300-53-6111
A300-53-6176
A300-53-6177
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-24-00 51-40-00 51-40-20
51-40-30 51-40-40 51-44-00
**CONF 003
Aircraft Maintenance Manual (AMM)
 06-21-00 06-31-53 06-41-00
06-41-53 20-21-12 20-28-11
24-00-00 28-00-00 28-10-00
28-11-29 28-13-21 28-25-00
32-12-11
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-51-20 20-55-00
Service Bulletin (SB)
 A300-53-6176
A300-53-6177
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-24-00 51-40-00 51-40-20
51-40-30 51-40-40 51-44-00
**CONF ALL
K. PUBLICATION AFFECTED
Structural Repair Manual (SRM)
 57-10-24
Impact on scheduled maintenance: Refer to MPD
L. INTERCHANGEABILITY/MIXABILITY
**CONF 001
NOTE
: The interchangeability/mixability possibilities are for new or modified parts
introduced by the accomplishment of this Service Bulletin.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 22
5
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### Page 29

@A300-600
SERVICE BULLETIN
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Frame foot
 A5711112900000
 A5711004100000
 03
 Not
Applicable
(1)
Frame foot
 A5711112900100
 A5711004100100
 03
 Not
Applicable
(1)
Frame foot
 A5711113000000
 A5711004200000
 03
 Not
Applicable
(1)
Frame foot
 A5711113000100
 A5711004200100
 03
 Not
Applicable
(1)
Frame foot
 A5711113100000
 A5711004300000
 03
 Not
Applicable
(1)
Frame foot
 A5711113100100
 A5711004300100
 03
 Not
Applicable
(1)
Frame foot
 A5711113200000
 A5711004400000
 03
 Not
Applicable
(1)
Frame foot
 A5711113200100
 A5711004400100
 03
 Not
Applicable
(1)
Frame foot
 A5711113300000
 A5711004500000
 03
 Not
Applicable
(1)
Frame foot
 A5711113300100
 A5711004500100
 03
 Not
Applicable
(1)
Frame foot
 A5711113400000
 A5711004600000
 03
 Not
Applicable
(1)
Frame foot
 A5711113400100
 A5711004600100
 03
 Not
Applicable
(1)
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
 (1)
: Interchangeability post-mod to pre-mod possible if all parts post-mod must be
replaced by parts pre-mod.
**CONF 002
NOTE
: The interchangeability/mixability possibilities are for new or modified parts
introduced by the accomplishment of this Service Bulletin.
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Frame foot
 A5711112900000
 A5711004100000
 03
 Not
Applicable
(1)
Frame foot
 A5711112900095
 A5711004100000
 03
 Not
Applicable
(1)
Frame foot
 A5711112900100
 A5711004100100
 03
 Not
Applicable
(1)
Frame foot
 A5711112900195
 A5711004100100
 03
 Not
Applicable
(1)
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 23
5
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### Page 30

@A300-600
SERVICE BULLETIN
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Frame foot
 A5711113000000
 A5711004200000
 03
 Not
Applicable
(1)
Frame foot
 A5711113000095
 A5711004200000
 03
 Not
Applicable
(1)
Frame foot
 A5711113000100
 A5711004200100
 03
 Not
Applicable
(1)
Frame foot
 A5711113000195
 A5711004200100
 03
 Not
Applicable
(1)
Frame foot
 A5711113100000
 A5711004300000
 03
 Not
Applicable
(1)
Frame foot
 A5711113100095
 A5711004300000
 03
 Not
Applicable
(1)
Frame foot
 A5711113100100
 A5711004300100
 03
 Not
Applicable
(1)
Frame foot
 A5711113100195
 A5711004300100
 03
 Not
Applicable
(1)
Frame foot
 A5711113200000
 A5711004400000
 03
 Not
Applicable
(1)
Frame foot
 A5711113200095
 A5711004400000
 03
 Not
Applicable
(1)
Frame foot
 A5711113200100
 A5711004400100
 03
 Not
Applicable
(1)
Frame foot
 A5711113200195
 A5711004400100
 03
 Not
Applicable
(1)
Frame foot
 A5711113300000
 A5711004500000
 03
 Not
Applicable
(1)
Frame foot
 A5711113300095
 A5711004500000
 03
 Not
Applicable
(1)
Frame foot
 A5711113300100
 A5711004500100
 03
 Not
Applicable
(1)
Frame foot
 A5711113300195
 A5711004500100
 03
 Not
Applicable
(1)
Frame foot
 A5711113400000
 A5711004600000
 03
 Not
Applicable
(1)
Frame foot
 A5711113400095
 A5711004600000
 03
 Not
Applicable
(1)
Frame foot
 A5711113400100
 A5711004600100
 03
 Not
Applicable
(1)
Frame foot
 A5711113400195
 A5711004600100
 03
 Not
Applicable
(1)
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 24
5
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### Page 31

@A300-600
SERVICE BULLETIN
NOTE
 (1)
: Interchangeability post-mod to pre-mod possible if all parts post-mod must be
replaced by parts pre-mod.
**CONF 003
NOTE
: The interchangeability/mixability possibilities are for new or modified parts
introduced by the accomplishment of this Service Bulletin.
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Frame foot
 A5711112900000
 A5711004100000
 03
 Not
Applicable
(1)
Frame foot
 A5711112900100
 A5711004100100
 03
 Not
Applicable
(1)
Frame foot
 A5711113000000
 A5711004200000
 03
 Not
Applicable
(1)
Frame foot
 A5711113100195
 A5711004200100
 03
 Not
Applicable
(1)
Frame foot
 A5711113100000
 A5711004300000
 03
 Not
Applicable
(1)
Frame foot
 A5711113100100
 A5711004300100
 03
 Not
Applicable
(1)
Frame foot
 A5711113200000
 A5711004400000
 03
 Not
Applicable
(1)
Frame foot
 A5711113200100
 A5711004400100
 03
 Not
Applicable
(1)
Frame foot
 A5711113300000
 A5711004500000
 03
 Not
Applicable
(1)
Frame foot
 A5711113300100
 A5711004500100
 03
 Not
Applicable
(1)
Frame foot
 A5711113400000
 A5711004600000
 03
 Not
Applicable
(1)
Frame foot
 A5711113400100
 A5711004600100
 03
 Not
Applicable
(1)
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
 (1)
: Interchangeability post-mod to pre-mod possible if all parts post-mod must be
replaced by parts pre-mod.
**CONF ALL
M. SPARES
None
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 25
5
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### Page 32

@A300-600
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 26
5
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### Page 33

@A300-600
SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Customers with aircraft shown in the effectivity of this Service Bulletin should send a
purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:
Kit 536176A01R01
Kit 536176A02R01
Kit 536176A03R01
Kit 536176A04R01
Kit 536176A05R01
Kit 536176A06R01
Kit 536176A07R01
Kit 536176A08R01
Kit 536176A09R01
Kit 536176A10R01
Kit 536176A11R01
Kit 536176A12R01
Kit 536176A13R01
Kit 536176A14R01
Kit 536176A15R01
Kit 536176A16R01
Kit 536176A17R01
Kit 536176A18R01
Kit 536176A19R01
Kit 536176A20R01
Kit 536176A21R01
Kit 536176A22R01
Kit 536176A23R01
Kit 536176A24R01
Kit 536176A25R01
Kit 536176A26R01
Kit 536176A27R01
Kit 536176A28R01
Kit 536176A29R01
Kit 536176A30R01
Kit 536176A31R01
Kit 536176A32R01
Kit 536176A33R01
Kit 536176A34R01
Kit 536176A35R01
Kit 536176A36R01
AIRBUS Material, Logistics and Suppliers
Weg beim Jaeger 150
D-22335 HAMBURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by fax: +49 40 50 76 2590
For ordering by E-mail: airbus.kit@airbus.com
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:
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 27
5
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### Page 34

@A300-600
SERVICE BULLETIN
Component COMPA01
Component COMPA02
Component COMPA03
Component COMPA04
Component COMPA05
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
Kit 536176A01R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A02R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A03R01
Cost
 11,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 28
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 35

@A300-600
SERVICE BULLETIN
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A04R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A05R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A06R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A07R01
Cost
 12,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 29
5
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### Page 36

@A300-600
SERVICE BULLETIN
Kit 536176A08R01
Cost
 12,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A09R01
Cost
 11,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A10R01
Cost
 12,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A11R01
Cost
 12,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A12R01
Cost
 11,500.00 USD
Availability
 180 calendar days from receipt of order
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 30
5
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### Page 37

@A300-600
SERVICE BULLETIN
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A13R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A14R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A15R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A16R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 31
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 38

@A300-600
SERVICE BULLETIN
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A17R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A18R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A19R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A20R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 32
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 39

@A300-600
SERVICE BULLETIN
Kit 536176A21R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A22R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A23R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A24R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A25R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 33
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 40

@A300-600
SERVICE BULLETIN
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A26R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A27R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A28R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A29R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 34
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 41

@A300-600
SERVICE BULLETIN
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A30R01
Cost
 10,500.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A31R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A32R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A33R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 35
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 42

@A300-600
SERVICE BULLETIN
Kit 536176A34R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A35R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 536176A36R01
Cost
 11,000.00 USD
Availability
 180 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Component COMPA01
Operator supplied standard hardware parts required to accomplish this Service Bulletin,
are to be supplied from the operator’s stock.
Component COMPA02
Operator supplied standard hardware parts required to accomplish this Service Bulletin,
are to be supplied from the operator’s stock.
Component COMPA03
Operator supplied standard hardware parts required to accomplish this Service Bulletin,
are to be supplied from the operator’s stock.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 36
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 43

@A300-600
SERVICE BULLETIN
Component COMPA04
Operator supplied standard hardware parts required to accomplish this Service Bulletin,
are to be supplied from the operator’s stock.
Component COMPA05
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
Kit 536176A01R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 9
 BOLT
21
 ASNA2529-3
 36
 NUT
22
 EN6115V3A8
 2
 BOLT
23
 EN6115V3A10
 3
 BOLT
24
 EN6115V3X7
 7
 BOLT
25
 EN6115V3X8
 5
 BOLT
26
 EN6115V3X10
 2
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 4
 NUT
34
 EN6114V5X10
 2
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 2
 BOLT
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
100
 A5711004100000
 1
 FRAME FT
 (100)
 A5711112900000
 03
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
106
 A5381133020000
 1
 SPLICE
107
 A5381133520000
 1
 SHIM
150
 A5741028020001
 1
 GUSSET
152
 A5741028320001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 37
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 44

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A02R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 16
 BOLT
21
 ASNA2529-3
 36
 NUT
22
 EN6115V3A8
 7
 BOLT
23
 EN6115V3A10
 5
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 4
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 2
 BOLT
39
 EN6114V5Y10
 2
 BOLT
47
 EN6115V3A5
 6
 BOLT
48
 EN6115V3A4
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
62
 EN6114V4Y9
 2
 BOLT
100
 A5711004100000
 1
 FRAME FT
 (100)
 A5711112900000
 03
(100)
 A5711112900095
 03
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
106
 A5381133020000
 1
 SPLICE
107
 A5381133520000
 1
 SHIM
150
 A5741028020001
 1
 GUSSET
152
 A5741028320001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 38
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 45

@A300-600
SERVICE BULLETIN
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A03R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
21
 ASNA2529-3
 36
 NUT
24
 EN6115V3X7
 16
 BOLT
25
 EN6115V3X8
 7
 BOLT
26
 EN6115V3X10
 5
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 4
 NUT
34
 EN6114V5X10
 2
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 2
 BOLT
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
100
 A5711004100000
 1
 FRAME FT
 (100)
 A5711112900000
 03
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
106
 A5381133020000
 1
 SPLICE
107
 A5381133520000
 1
 SHIM
150
 A5741028020001
 1
 GUSSET
152
 A5741028320001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A04R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 39
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 46

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 9
 BOLT
21
 ASNA2529-3
 36
 NUT
22
 EN6115V3A8
 2
 BOLT
23
 EN6115V3A10
 3
 BOLT
24
 EN6115V3X7
 7
 BOLT
25
 EN6115V3X8
 5
 BOLT
26
 EN6115V3X10
 2
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 4
 NUT
34
 EN6114V5X10
 2
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 2
 BOLT
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
101
 A5711004100100
 1
 FRAME FT
 (101)
 A5711112900100
 03
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 1
 SHIM
105
 A5381133020100
 1
 SPLICE
107
 A5381133520000
 1
 SHIM
151
 A5741028020101
 1
 GUSSET
153
 A5741028320101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A05R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 16
 BOLT
21
 ASNA2529-3
 36
 NUT
22
 EN6115V3A8
 7
 BOLT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 40
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 47

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
23
 EN6115V3A10
 5
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 4
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 2
 BOLT
39
 EN6114V5Y10
 2
 BOLT
47
 EN6115V3A5
 6
 BOLT
48
 EN6115V3A4
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
62
 EN6114V4Y9
 2
 BOLT
101
 A5711004100100
 1
 FRAME FT
 (101)
 A5711112900100
 03
(101)
 A5711112900195
 03
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 1
 SHIM
105
 A5381133020100
 1
 SPLICE
107
 A5381133520000
 1
 SHIM
151
 A5741028020101
 1
 GUSSET
153
 A5741028320101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A06R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
21
 ASNA2529-3
 36
 NUT
24
 EN6115V3X7
 16
 BOLT
25
 EN6115V3X8
 7
 BOLT
26
 EN6115V3X10
 5
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 41
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 48

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 4
 NUT
34
 EN6114V5X10
 2
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 2
 BOLT
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
101
 A5711004100100
 1
 FRAME FT
 (101)
 A5711112900100
 03
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 1
 SHIM
105
 A5381133020100
 1
 SPLICE
107
 A5381133520000
 1
 SHIM
151
 A5741028020101
 1
 GUSSET
153
 A5741028320101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A07R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 4
 RIVET
20
 EN6115V3A7
 14
 BOLT
21
 ASNA2529-3
 48
 NUT
22
 EN6115V3A8
 8
 BOLT
23
 EN6115V3A10
 4
 BOLT
24
 EN6115V3X7
 10
 BOLT
26
 EN6115V3X10
 2
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 4
 BOLT
33
 ASNA2529-5
 8
 NUT
34
 EN6114V5X10
 4
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 4
 BOLT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 42
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 49

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
42
 ASNA2050DXJ4828
 3
 RIVET
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 5
 SHIM
114
 A5711004200000
 1
 FRAME FT
 (114)
 A5711113000000
 03
116
 A5381133920000
 1
 STFFNR
118
 A5381133120000
 1
 SPLICE
119
 A5381133620000
 1
 SHIM
154
 A5741028420001
 1
 GUSSET
156
 A5741028720001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A08R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 4
 RIVET
20
 EN6115V3A7
 21
 BOLT
21
 ASNA2529-3
 48
 NUT
22
 EN6115V3A8
 8
 BOLT
23
 EN6115V3A10
 4
 BOLT
24
 EN6115V3X7
 3
 BOLT
26
 EN6115V3X10
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 8
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 4
 BOLT
39
 EN6114V5Y10
 4
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 4
 BOLT
42
 ASNA2050DXJ4828
 3
 RIVET
61
 ASNA2529-4
 2
 NUT
62
 EN6114V4Y9
 2
 BOLT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 43
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 50

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 5
 SHIM
114
 A5711004200000
 1
 FRAME FT
 (114)
 A5711113000000
 03
(114)
 A5711113000095
 03
116
 A5381133920000
 1
 STFFNR
118
 A5381133120000
 1
 SPLICE
119
 A5381133620000
 1
 SHIM
154
 A5741028420001
 1
 GUSSET
156
 A5741028720001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A09R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 4
 RIVET
21
 ASNA2529-3
 48
 NUT
24
 EN6115V3X7
 24
 BOLT
25
 EN6115V3X8
 8
 BOLT
26
 EN6115V3X10
 6
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 4
 BOLT
33
 ASNA2529-5
 8
 NUT
34
 EN6114V5X10
 4
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 4
 BOLT
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 5
 SHIM
114
 A5711004200000
 1
 FRAME FT
 (114)
 A5711113000000
 03
116
 A5381133920000
 1
 STFFNR
118
 A5381133120000
 1
 SPLICE
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 44
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 51

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
119
 A5381133620000
 1
 SHIM
154
 A5741028420001
 1
 GUSSET
156
 A5741028720001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A10R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 4
 RIVET
20
 EN6115V3A7
 14
 BOLT
21
 ASNA2529-3
 48
 NUT
22
 EN6115V3A8
 8
 BOLT
23
 EN6115V3A10
 4
 BOLT
24
 EN6115V3X7
 10
 BOLT
26
 EN6115V3X10
 2
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 4
 BOLT
33
 ASNA2529-5
 8
 NUT
34
 EN6114V5X10
 4
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 4
 BOLT
42
 ASNA2050DXJ4828
 3
 RIVET
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 5
 SHIM
113
 A5711004200100
 1
 FRAME FT
 (113)
 A5711113000100
 03
115
 A5381133920100
 1
 STFFNR
117
 A5381133120100
 1
 SPLICE
119
 A5381133620000
 1
 SHIM
155
 A5741028420101
 1
 GUSSET
157
 A5741028720101
 1
 GUSSET
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 45
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 52

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A11R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 4
 RIVET
20
 EN6115V3A7
 21
 BOLT
21
 ASNA2529-3
 48
 NUT
22
 EN6115V3A8
 8
 BOLT
23
 EN6115V3A10
 4
 BOLT
24
 EN6115V3X7
 3
 BOLT
26
 EN6115V3X10
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 8
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 4
 BOLT
39
 EN6114V5Y10
 4
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 4
 BOLT
42
 ASNA2050DXJ4828
 3
 RIVET
61
 ASNA2529-4
 2
 NUT
62
 EN6114V4Y9
 2
 BOLT
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 5
 SHIM
113
 A5711004200100
 1
 FRAME FT
 (113)
 A5711113000100
 03
(113)
 A5711113000195
 03
115
 A5381133920100
 1
 STFFNR
117
 A5381133120100
 1
 SPLICE
119
 A5381133620000
 1
 SHIM
155
 A5741028420101
 1
 GUSSET
157
 A5741028720101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 46
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 53

@A300-600
SERVICE BULLETIN
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A12R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 4
 RIVET
21
 ASNA2529-3
 48
 NUT
24
 EN6115V3X7
 24
 BOLT
25
 EN6115V3X8
 8
 BOLT
26
 EN6115V3X10
 6
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 4
 BOLT
33
 ASNA2529-5
 8
 NUT
34
 EN6114V5X10
 4
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 4
 BOLT
60
 EN6114V4X9
 2
 BOLT
61
 ASNA2529-4
 2
 NUT
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 5
 SHIM
113
 A5711004200100
 1
 FRAME FT
 (123)
 A5711113100195
 03
115
 A5381133920100
 1
 STFFNR
117
 A5381133120100
 1
 SPLICE
119
 A5381133620000
 1
 SHIM
155
 A5741028420101
 1
 GUSSET
157
 A5741028720101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 47
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 54

@A300-600
SERVICE BULLETIN
Kit 536176A13R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 11
 BOLT
21
 ASNA2529-3
 39
 NUT
22
 EN6115V3A8
 2
 BOLT
24
 EN6115V3X7
 5
 BOLT
25
 EN6115V3X8
 6
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 5
 NUT
34
 EN6114V5X10
 3
 BOLT
40
 EN6115V3X5
 4
 BOLT
43
 EN6115V3X9
 6
 BOLT
44
 EN6115V3A11
 3
 BOLT
46
 EN6115V3X11
 2
 BOLT
60
 EN6114V4X9
 1
 BOLT
61
 ASNA2529-4
 1
 NUT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
122
 A5381133220000
 1
 SPLICE
124
 A5711004300000
 1
 FRAME FT
 (124)
 A5711113100000
 03
125
 A5381133720000
 1
 SHIM
158
 A5741028820001
 1
 GUSSET
160
 A5741029120001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A14R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 16
 BOLT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 48
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 55

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
21
 ASNA2529-3
 39
 NUT
22
 EN6115V3A8
 8
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 5
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 2
 BOLT
39
 EN6114V5Y10
 3
 BOLT
44
 EN6115V3A11
 5
 BOLT
45
 EN6115V3A9
 6
 BOLT
47
 EN6115V3A5
 4
 BOLT
61
 ASNA2529-4
 1
 NUT
62
 EN6114V4Y9
 1
 BOLT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
122
 A5381133220000
 1
 SPLICE
124
 A5711004300000
 1
 FRAME FT
 (124)
 A5711113100000
 03
(124)
 A5711113100095
 03
125
 A5381133720000
 1
 SHIM
158
 A5741028820001
 1
 GUSSET
160
 A5741029120001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A15R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
21
 ASNA2529-3
 39
 NUT
24
 EN6115V3X7
 16
 BOLT
25
 EN6115V3X8
 8
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 49
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 56

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 5
 NUT
34
 EN6114V5X10
 3
 BOLT
40
 EN6115V3X5
 4
 BOLT
43
 EN6115V3X9
 6
 BOLT
46
 EN6115V3X11
 5
 BOLT
60
 EN6114V4X9
 1
 BOLT
61
 ASNA2529-4
 1
 NUT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
122
 A5381133220000
 1
 SPLICE
124
 A5711004300000
 1
 FRAME FT
 (124)
 A5711113100000
 03
125
 A5381133720000
 1
 SHIM
158
 A5741028820001
 1
 GUSSET
160
 A5741029120001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A16R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 11
 BOLT
21
 ASNA2529-3
 39
 NUT
22
 EN6115V3A8
 2
 BOLT
24
 EN6115V3X7
 5
 BOLT
25
 EN6115V3X8
 6
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 5
 NUT
34
 EN6114V5X10
 3
 BOLT
40
 EN6115V3X5
 4
 BOLT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 50
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 57

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
43
 EN6115V3X9
 6
 BOLT
44
 EN6115V3A11
 3
 BOLT
46
 EN6115V3X11
 2
 BOLT
60
 EN6114V4X9
 1
 BOLT
61
 ASNA2529-4
 1
 NUT
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
121
 A5381133220100
 1
 SPLICE
123
 A5711004300100
 1
 FRAME FT
 (123)
 A5711113100100
 03
125
 A5381133720000
 1
 SHIM
159
 A5741028820101
 1
 GUSSET
161
 A5741029120101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A17R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 16
 BOLT
21
 ASNA2529-3
 39
 NUT
22
 EN6115V3A8
 8
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 5
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 2
 BOLT
39
 EN6114V5Y10
 3
 BOLT
44
 EN6115V3A11
 5
 BOLT
45
 EN6115V3A9
 6
 BOLT
47
 EN6115V3A5
 4
 BOLT
61
 ASNA2529-4
 1
 NUT
62
 EN6114V4Y9
 1
 BOLT
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 51
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 58

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
121
 A5381133220100
 1
 SPLICE
123
 A5711004300100
 1
 FRAME FT
 (123)
 A5711113100100
 03
(123)
 A5711113100195
 03
125
 A5381133720000
 1
 SHIM
159
 A5741028820101
 1
 GUSSET
161
 A5741029120101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A18R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
21
 ASNA2529-3
 39
 NUT
24
 EN6115V3X7
 16
 BOLT
25
 EN6115V3X8
 8
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 2
 BOLT
33
 ASNA2529-5
 4
 NUT
34
 EN6114V5X10
 3
 BOLT
40
 EN6115V3X5
 4
 BOLT
43
 EN6115V3X9
 6
 BOLT
46
 EN6115V3X11
 5
 BOLT
60
 EN6114V4X9
 1
 BOLT
61
 ASNA2529-4
 1
 NUT
103
 A5381133820100
 1
 STFFNR
104
 A5381134020000
 3
 SHIM
121
 A5381133220100
 1
 SPLICE
123
 A5711004300100
 1
 FRAME FT
 (123)
 A5711113100100
 03
125
 A5381133720000
 1
 SHIM
159
 A5741028820101
 1
 GUSSET
161
 A5741029120101
 1
 GUSSET
175
 MS21051L3
 4
 NUT
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 52
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 59

@A300-600
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A19R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 10
 BOLT
21
 ASNA2529-3
 35
 NUT
22
 EN6115V3A8
 2
 BOLT
23
 EN6115V3A10
 3
 BOLT
24
 EN6115V3X7
 5
 BOLT
25
 EN6115V3X8
 5
 BOLT
26
 EN6115V3X10
 2
 BOLT
27
 EN6114V6X14
 2
 BOLT
28
 ASNA2529-6
 2
 NUT
29
 ASNA2001V5-8X
 1
 SCREW
30
 NAS1726-5E
 2
 NUT
31
 ASNA2001V5-10X
 1
 SCREW
32
 EN6114V5X8
 1
 BOLT
33
 ASNA2529-5
 4
 NUT
34
 EN6114V5X10
 3
 BOLT
40
 EN6115V3X5
 6
 BOLT
41
 EN6115V3X4
 2
 BOLT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 2
 SHIM
107
 A5381133520000
 1
 SHIM
130
 A5711004400000
 1
 FRAME FT
 (130)
 A5711113200000
 03
134
 A5381133320000
 1
 SPLICE
162
 A5741029220001
 1
 GUSSET
164
 A5741029520001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 53
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 60

@A300-600
SERVICE BULLETIN
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A20R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
20
 EN6115V3A7
 15
 BOLT
21
 ASNA2529-3
 35
 NUT
22
 EN6115V3A8
 7
 BOLT
23
 EN6115V3A10
 5
 BOLT
28
 ASNA2529-6
 2
 NUT
30
 NAS1726-5E
 2
 NUT
33
 ASNA2529-5
 4
 NUT
35
 EN6114V6Y14
 2
 BOLT
36
 ASNA2001V5-8Y
 1
 SCREW
37
 ASNA2001V5-10Y
 1
 SCREW
38
 EN6114V5Y8
 1
 BOLT
39
 EN6114V5Y10
 3
 BOLT
47
 EN6115V3A5
 6
 BOLT
48
 EN6115V3A4
 2
 BOLT
102
 A5381133820000
 1
 STFFNR
104
 A5381134020000
 2
 SHIM
107
 A5381133520000
 1
 SHIM
130
 A5711004400000
 1
 FRAME FT
 (130)
 A5711113200000
 03
(130)
 A5711113200095
 03
134
 A5381133320000
 1
 SPLICE
162
 A5741029220001
 1
 GUSSET
164
 A5741029520001
 1
 GUSSET
175
 MS21051L3
 4
 NUT
176
 ASNA2051DCJ2430
 8
 RIVET
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 536176A21R01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 NSA5057-6
 4
 NUT
15
 ASNA2050DXJ4020
 2
 RIVET
DATE: May 20/15 SERVICE BULLETIN No.: A300-53-6176
REVISION No.: 00 - May 20/15 Page: 54
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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