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@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.
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 57 TITLE: WINGS - CENTER WINGS - INSPECTION OF FRAME 40 LOWER
OUTBOARD RADIUS FOR CRACKS **CONF ALL
MODIFICATIONS None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Further to in-service findings, mandatory Inspection Service Bulletin No. A300-57-6052 was issued to inspect the lower outboard radius of frame 40 forward fitting. In addition, Modification Service Bulletin No. A300-57-6053 was proposed as a terminating action of Inspection Service Bulletin No.
A300-57-6052, either as a corrective or preventive action. Recent crack findings on post-Service Bulletin No. A300-57-6053 aircraft and a new extensive study led Airbus to define new inspection for all aircraft with or without Service Bulletin No. A300-57-6053 applied.
The Service Bulletin No. A300-57-6053 is no longer considered as a terminative action of Inspection Service Bulletin No. A300-57-6052.
This new Inspection Service Bulletin cancels and supersedes the Inspection Service Bulletin No.
A300-57-6052. It proposes repair solutions depending on crack length, and their associated inspection program. In addition new areas must also be inspected inside the Center Wing Box for aircraft with Service Bulletin No. A300-57-6053 embodied.
Accomplishment of this Inspection Service Bulletin will allow early detection of cracks avoiding long cracks which can lead to costly and time-consuming repairs.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
DE-FUELING/VENTILATION YES NOTE
(1) : Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION **CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 576117A01R00 2
314.00 Bolt, Nut Kit 576117A02R00 2 1,132.00 Bolt, Nut Kit 576117A03R00 2 3,580.00 Bolt, Nut Kit 576117A04R00 2 1,236.00 Bolt, Nut Kit 576117A05R00 2
754.00 Bolt, Nut Kit 576117A06R00 1
293.00 Bolt, Nut Kit 576117A07R00 2
356.00 Bolt, Nut Kit 576117A08R00 2 1,236.00 Bolt, Nut Kit 576117A09R00 1
335.00 Bolt, Nut Kit 576117A10R00 2
104.80 Bolt, Nut TOTAL 9,340.80 **CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 576117A06R00 1
293.00 Bolt, Nut Kit 576117A05R00 2
754.00 Bolt, Nut Kit 576117A09R00 1
335.00 Bolt, Nut Kit 576117A10R00 2
104.80 Bolt, Nut TOTAL 1,486.80 **CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 576117A06R00 1
293.00 Bolt, Nut Kit 576117A05R00 2
754.00 Bolt, Nut Kit 576117A09R00 1
335.00 Bolt, Nut TOTAL 1,382.00 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 004
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 576117A01R00 2
314.00 Bolt, Nut Kit 576117A02R00 2 1,132.00 Bolt, Nut Kit 576117A03R00 2 3,580.00 Bolt, Nut Kit 576117A04R00 2 1,236.00 Bolt, Nut Kit 576117A05R00 2
754.00 Bolt, Nut Kit 576117A06R00 1
293.00 Bolt, Nut Kit 576117A07R00 2
356.00 Bolt, Nut Kit 576117A08R00 2 1,236.00 Bolt, Nut Kit 576117A09R00 1
335.00 Bolt, Nut Kit 576117A10R00 2
104.80 Bolt, Nut TOTAL 9,340.80 **CONF 005
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 576117A06R00 1
293.00 Bolt, Nut Kit 576117A05R00 2
754.00 Bolt, Nut Kit 576117A09R00 1
335.00 Bolt, Nut TOTAL 1,382.00 **CONF 006 No Material
EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :
67Q ABR AHK BCS F2I FDX IRA IRM KAC MNB MSR SUD TAR
T H AU Q A U T PU Z B
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU
57.10.00.006 OEB None AOT None DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY 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 576117-839-801-001: Contact and Report to AIRBUS
TOTAL MANHOURS
0.00 Task 576117-832-801-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius For Cracks for LH and RH Sides
TOTAL MANHOURS
91.00
ELAPSED TIME (HOURS)
45.00 Task 576117-832-802-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius for Cracks After Repair for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 Task 576117-832-804-001: Special Detailed Inspections of the Surrounding Area of the Repair for Cracks for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-805-001: Special Detailed Inspection of the Surrounding Area of the Rework for Cracks for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-808-001: Rototest Inspection of Fastener Hole in Area of Rib 1 Triform in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-806-001: Rototest Inspection of Fastener Holes in the Front Spar Lower Flange area in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
39.00
ELAPSED TIME (HOURS)
19.50 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY Task 576117-832-809-001: Ultrasonic Inspection of Center Wing Box Lower Panel Area for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 **CONF 002 Task 576117-839-801-001: Contact and Report to AIRBUS
TOTAL MANHOURS
0.00 Task 576117-832-801-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius For Cracks for LH and RH Sides
TOTAL MANHOURS
35.00
ELAPSED TIME (HOURS)
17.50 Task 576117-832-804-001: Special Detailed Inspections of the Surrounding Area of the Repair for Cracks for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-808-001: Rototest Inspection of Fastener Hole in Area of Rib 1 Triform in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-806-001: Rototest Inspection of Fastener Holes in the Front Spar Lower Flange area in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
39.00
ELAPSED TIME (HOURS)
19.50 Task 576117-832-809-001: Ultrasonic Inspection of Center Wing Box Lower Panel Area for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 **CONF 003 Task 576117-839-801-001: Contact and Report to AIRBUS
TOTAL MANHOURS
0.00 Task 576117-832-801-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius For Cracks for LH and RH Sides
TOTAL MANHOURS
35.00
ELAPSED TIME (HOURS)
17.50 Task 576117-832-805-001: Special Detailed Inspection of the Surrounding Area of the Rework for Cracks for LH and RH Sides
TOTAL MANHOURS
34.00 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY Task 576117-832-805-001: Special Detailed Inspection of the Surrounding Area of the Rework for Cracks for LH and RH Sides
ELAPSED TIME (HOURS)
17.00 Task 576117-832-808-001: Rototest Inspection of Fastener Hole in Area of Rib 1 Triform in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-806-001: Rototest Inspection of Fastener Holes in the Front Spar Lower Flange area in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
39.00
ELAPSED TIME (HOURS)
19.50 Task 576117-832-809-001: Ultrasonic Inspection of Center Wing Box Lower Panel Area for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 **CONF 004 Task 576117-839-801-001: Contact and Report to AIRBUS
TOTAL MANHOURS
0.00 Task 576117-832-801-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius For Cracks for LH and RH Sides
TOTAL MANHOURS
90.75
ELAPSED TIME (HOURS)
45.00 Task 576117-832-802-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius for Cracks After Repair for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 Task 576117-832-804-001: Special Detailed Inspections of the Surrounding Area of the Repair for Cracks for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-805-001: Special Detailed Inspection of the Surrounding Area of the Rework for Cracks for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-808-001: Rototest Inspection of Fastener Hole in Area of Rib 1 Triform in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY Task 576117-832-806-001: Rototest Inspection of Fastener Holes in the Front Spar Lower Flange area in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
39.00
ELAPSED TIME (HOURS)
19.50 Task 576117-832-809-001: Ultrasonic Inspection of Center Wing Box Lower Panel Area for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 **CONF 005 Task 576117-839-801-001: Contact and Report to AIRBUS
TOTAL MANHOURS
0.00 Task 576117-832-801-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius For Cracks for LH and RH Sides
TOTAL MANHOURS
33.00
ELAPSED TIME (HOURS)
16.50 Task 576117-832-802-001: Special Detailed Inspection of Frame 40 Lower Outboard Radius for Cracks After Repair for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 Task 576117-832-808-001: Rototest Inspection of Fastener Hole in Area of Rib 1 Triform in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
34.00
ELAPSED TIME (HOURS)
17.00 Task 576117-832-806-001: Rototest Inspection of Fastener Holes in the Front Spar Lower Flange area in the Center Wing Box for LH and RH Sides
TOTAL MANHOURS
39.00
ELAPSED TIME (HOURS)
19.50 Task 576117-832-809-001: Ultrasonic Inspection of Center Wing Box Lower Panel Area for LH and RH Sides
TOTAL MANHOURS
32.00
ELAPSED TIME (HOURS)
16.00 **CONF 006 Task 576117-839-801-001: Contact and Report to AIRBUS
TOTAL MANHOURS
0.50
ELAPSED TIME (HOURS)
0.50 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY
APPENDICES **CONF ALL Appendix 01 - NTM Task 57-10-36 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 001, 004 B B B
RH SHOWN
LH SYMMETRICAL
FRONT SPAR DATUM RIB1 DATUM FR40 FR47 A FR40 C Z140 A D_SB_576117_5_SAAA_01_00 Figure A-FSAAA - Sheet 01 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 9 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 001, 004 C
VIEW LOOKING AFT
RH SHOWN
LH SYMMETRICAL STGR33 STGR32
AREA TO BE INSPECTED
DO A ROTOTEST INSPECTION OF THE HOLE NOTE:
AREA AAREA B
TYPICAL CRACK D_SB_576117_5_SAAA_02_01 Figure A-FSAAA - Sheet 02 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 10 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 002 thru 005 B B FR40 FR47 A
RH SHOWN
LH SYMMETRICAL B
RH SHOWN
LH SYMMETRICAL
FRONT SPAR DATUM RIB1 DATUM FR40 C C FR40 Z140 A D E D_SB_576117_5_SBAA_01_00 Figure A-FSBAA - Sheet 01 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 11 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY **CONF 002 thru 005
VIEW LOOKING FWD
LH SHOWN
RH SYMMETRICAL OUTBD
DO A ROTOTEST INSPECTION OF THE HOLE
FASTENERS NOT AFFECTED NOTE:
H1 H2 H3 H4 H6 H5
VIEW LOOKING DOWN OUTBD H7
AREA TO BE INSPECTED F W D D E
RH SYMMETRICAL
LH SHOWN D_SB_576117_5_SBAA_02_00 Figure A-FSBAA - Sheet 02 DATE: May 28/15 SERVICE BULLETIN No.: A300-57-6117 REVISION No.: 00 - May 28/15 Page: 12 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.