(2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.
Subtask 57-53-00-865-127
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 57-53-00-010-084
D. Get Access
(1)
Put the access platform in position below the flap track 3 at zone 587(687).
(2)
Remove the applicable flap track fairing (Ref. TASK 57-55-11-000-004):
-
for the left wing, remove 532AT, 532CB
-
for the right wing, remove 632AT, 632CB.
(3)
Put the spark-proof lamp adjacent to the inspection area.
4. Procedure
_________
(Ref. Fig. 633/TASK 57-53-00-991-037)
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 57-53-00-110-088
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the tab lever, tab bracket, aft flap bracket, drive strut and tab rear link.
1EFF : 301-399, 1 57-53-00Page B626 1 1 Nov 01/04R 1 1 1CES 1
Outboard Flap - Tab Articulation at Track 3 -Inspection Area
Figure 633/TASK 57-53-00-991-037
R 1EFF : 301-399, 1 57-53-00Page B627 1 1 Nov 01/04 1 1 1CES 1 Subtask 57-53-00-210-076
B. Inspection.
(1)
Do an inspection of the tab lever, the tab bracket and the aft flap bracket. Make sure that:
-
there is no damage
-
there is no corrosion
-
there are no cracks or scores
-the surface protection is in the correct condition.
(2)
Do an inspection of the drive strut and tab rear link. Make sure that:
-
there is no damage
-
there is no corrosion
-they are attached correctly.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____
correct repair procedure.
5. Close-up
________
Subtask 57-53-00-410-083
A. Close Access
(1)
Remove the spark-proof lamp from the inspection area.
(2)
Install the applicable flap track fairing (Ref. TASK 57-55-11-400-004):
-
for the left wing, install 532AT, 532CB
-
for the right wing, install 632AT, 632CB.
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 57-53-00-865-128
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-53-00-860-071
C. Aircraft Maintenance Configuration
(1) Fully retract the flaps (Ref. TASK 27-50-00-866-009).
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D. Removal of Equipment
(1)
Remove the access platform(s).
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : 301-399, 1 57-53-00Page B629 1 1 Nov 01/04R 1 1 1CES 1
TASK 57-53-00-220-018
Special Detailed Inspection of Outboard Double Slotted Flap, Tab Articulation at Track 3, LH/RH
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
中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼5(22)
