R MLG Reinforcing Plate - Inspection Area Figure 631/TASK 57-20-00-991-039
1EFF : 1 1 1CES ALL 1 111 57-20-00 Page A667 Aug 01/05
Subtask 57-20-00-210-080
B. Inspection
(1) Make a visual inspection of the surface area of the MLG reinforcing plate. Make sure that:
-
there is no damage
-
there are no cracks
-
there is no corrosion
-the paint finish is in the correct condition.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 572000) for the
____
correct repair procedure.
5. Close-up
________ Subtask 57-20-00-942-090
A. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 57-20-00Page A668 1 1 Aug 01/05R 1 1 1CES 1
TASK 57-20-00-210-004
General Visual Inspection of Outer Wing, Bottom Skin Lower Surface Spanwise Skin Joints at Stringer 8 and Stringer 11, between Rib 1 and Rib 8, ...
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: 572044-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adjustable access platform No specific safety barriers No specific warning notices 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 A669 1 1 Aug 01/05R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 572000 (for corrective action) R 57-20-00-991-040 Fig. 632
3. Job Set-up
__________
Subtask 57-20-00-941-090
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(3)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-20-00-010-087
B. Get Access
(1) Put the adjustable access platform in position at the applicable zone 500(600).
4. Procedure
_________ R (Ref. Fig. 632/TASK 57-20-00-991-040) Subtask 57-20-00-100-051
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the applicable area for inspection.
Bottom Skin, Lower Surface at Stringer 8 and Stringer 11, between Rib 1 and Rib 8 R Figure 632/TASK 57-20-00-991-040
Subtask 57-20-00-210-077
B. General Visual Inspection of Outer Wing, Lower Surface Spanwise Skin Joints at Stringer 8 and Stringer 11, between Rib 1 and Rib 8, excluding Areas covered by Reinforcing Plate and Fairings.
(1) Do an inspection and make sure that:
-
there is no damage
-
there are no cracks
-
there is no corrosion
-the paint finish is in the correct condition.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 572000) 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飛機維護(hù)手冊 AMM WINGS 機翼1(110)
