-
the paint finishes are correct.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 572100) for the
____
correct repair procedure.
5. Close-up
________
Subtask 57-20-00-410-051
A. Close Access
(1) Install the fuel pumps 21QA(26QA) and 25QA(22QA) (Ref. TASK 28-21-51-400-001).
R Fuel Pump 25QA (22QA) 21QA (26QA) Openings Figure 603/TASK 57-20-00-991-002
1EFF : 1 1 1CES ALL 1 111 57-20-00 Page 619 Aug 01/05
Subtask 57-20-00-942-084
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 57-20-00Page 620 1 1 Aug 01/05R 1 1 1CES 1
TASK 57-20-00-220-001
Detailed Inspection of Outer Wing, Top Skin Upper Surface at Attachment to Front Spar and Rear Spar, between RIB1 and RIB8
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
Refer to the MPD TASK: 572012-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notices No specific access platform 3 m (9 ft. 10 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
1EFF : ALL 1 57-20-00Page 621 1 1 Aug 01/05R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
12-00-00-081-001 Removal of the Wing Safety Rope
12-00-00-481-001 Installation of the Wing Safety Rope
ASRM 572100 (for corrective action)
R 57-20-00-991-003 Fig. 604
3. Job Set-up
__________
Subtask 57-20-00-941-051
A. Safety Precautions
(1)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(2)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(3)
Put the access platform in position below zone 500(600).
(4)
Put the safety barriers in position.
(5)
Install the wing safety rope (Ref. TASK 12-00-00-481-001).
4. Procedure
_________ R (Ref. Fig. 604/TASK 57-20-00-991-003) Subtask 57-20-00-110-052
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 wing top-skin at its joint between the front spar and the rear spar from RIB1 to RIB8.
R Top View of the Wing Upper Skin - RIB1 thru RIB8 Figure 604/TASK 57-20-00-991-003
1EFF : 1 1 1CES ALL 1 111 57-20-00 Page 623 Aug 01/05
Subtask 57-20-00-220-050
B. Detailed Visual Inspection of the Outer Wing Top-Skin Surface at the Attachment to the Front Spar between RIB1 and RIB8
(1) Inspect the upper surface of the wing top-skin at its attachment to the front spar and the rear spar (between RIB1 and RIB8). Make sure that:
-
there is no corrosion
-
there are no dents, burrs, scores or scratches
-
the rivets and fasteners are in the correct condition
-
the surface protection is not damaged or loose.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 572100) for the
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM WINGS 機(jī)翼1(74)
