R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-20-00Page 661 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 B. Consumable Materials
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Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
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28-00-00-910-001 Fuel Safety Procedures 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank 57-27-11-000-001 Removal of the Access Panel (540AB, 540BB, 540CB,
540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB,
640DB, 640EB, 640FB, 640GB)
57-27-11-000-003 Removal of the Closing Panel 540CZ
57-27-11-000-007 Removal of the Closing Panel
540CZ(640CZ),540DZ(640DZ)
57-27-11-400-001 Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
57-27-11-400-003 Installation of the Closing Panel 540CZ 57-27-11-400-007 Installation of the Closing Panel 540CZ(640CZ), 540DZ(640DZ) ASRM 572100 (for corrective action) R 57-20-00-991-011 Fig. 612
3. Job Set-up
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Subtask 57-20-00-941-059
A. Safety Precautions
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
(1)
Obey the fuel safety precautions (Ref. TASK 28-00-00-910-001) and (Ref. TASK 28-10-00-910-001).
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
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(3)
Put warning notices in the cockpit to tell persons not to operate the
flaps or slats.
(4)
Put the safety barriers in position.
Subtask 57-20-00-010-059
B. Get Access
WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
(1)
Put the access platform below the access panels 540AB (640AB) and 540BB (640BB).
(2)
Remove the applicable access panels:
-
for the left wing, remove 540AB, 540BB, 540CZ, 540DZ
-
for the right wing, remove 640AB, 640BB, 640CZ, 640DZ, (Ref. TASK 57-27-11-000-001), (Ref. TASK 57-27-11-000-003) and (Ref. TASK 57-27-11-000-007).
(3)
Open the RIB2 surge doors:
-
for the left wing, open 540AZ, 540BZ
-
for the right wing, open 640AZ, 640BZ.
(4)
Install the HOOK-COVER (RIB 2 SURGE DOORS) (98D57004013000) on the forward surge doors.
(5)
Install the HOOK-COVER (RIB2-SURGE DOORS) (98D57004014000) on the aft surge doors.
4. Procedure
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R (Ref. Fig. 612/TASK 57-20-00-991-011)
Subtask 57-20-00-110-060
A. Preparation for Inspection
(1) Use a clean MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026), to clean:
-
the top skin stringers between RIB1 and RIB8. Make sure that you clean:
-
the runouts
-
the area around each air transfer hole
-
the stringer joints
-
the buttstrap at stringer 11.
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R Details of the Top Skin Stringers - RIB1 thru RIB8 Figure 612/TASK 57-20-00-991-011
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Subtask 57-20-00-210-058
B. Detailed Inspection of Outer Wing, Top-Skin Stringers, Between RIB1 and RIB8, including the Runouts and Air Transfer Holes, Stringer Joints, and Butt Strap, at Stringer 11 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼1(84)
