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时间:2011-03-27 12:52来源:蓝天飞行翻译 作者:航空
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 Subtask 57-53-00-865-123
 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 57-53-00-010-082
 D. Get Access
 (1)
 Put the access platform in position below the applicable tab hinge-fairing at zone 587(687).

 (2)
 Remove the applicable tab hinge-fairing (Ref. TASK 57-55-11-000-005):

 -
for the left wing, remove 537AB, 537BB, 537CB, 538AB, 538BB, 538CB, 539AB, 539BB, 539CB

 -
for the right wing, remove 637AB, 637BB, 637CB, 638AB, 638BB, 638CB, 639AB, 639BB, 639CB.

 

 (3)
 Put the spark-proof lamp adjacent to the inspection area.


 4. Procedure
_________
 (Ref. Fig. 631/TASK 57-53-00-991-035)
 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 57-53-00-110-086
 A. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the outboard double slotted flap, tab articulation at stations 3A, 3B, 3C.
 1EFF : 301-399, 1 57-53-00Page B614 1 1 Nov 01/04R 1 1 1CES 1


 Outboard Flap - Tab Articulation - Inspection Area
 Figure 631/TASK 57-53-00-991-035

 1EFF : 301-399, 1 57-53-00Page B615 1 1 Nov 01/04R 1 1 1CES 1


 Subtask 57-53-00-210-075
 B. Detailed Visual Inspection of Outboard Double Slotted Flap, Tab
 Articulation at Stations 3A, 3B, 3C

 (1)
 Do an inspection of the support strut, the forward link and the rear link. Make sure that:

 -
there is no damage

 -
there is no corrosion

 -
there are no cracks or scores


 -they are attached correctly.

 (2)
 Do an inspection of 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.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____
 correct repair procedure.

 5. Close-up
________
 Subtask 57-53-00-410-081
 A. Close Access
 (1)
 Remove the spark-proof lamp from the inspection area.

 (2)
 Install the applicable tab hinge-fairing (Ref. TASK 57-55-11-400-005):

 -
for the left wing, install 537AB, 537BB, 537CB, 538AB, 538BB, 538CB, 539AB, 539BB, 539CB

 -
for the right wing, install 637AB, 637BB, 637CB, 638AB, 638BB, 638CB, 639AB, 639BB, 639CB.

 

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.


 Subtask 57-53-00-865-124
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 1EFF : 301-399, 1 57-53-00Page B616 1 1 Nov 01/04R 1 1 1CES 1


 Subtask 57-53-00-860-067
 C. Aircraft Maintenance Configuration
 (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-53-00-942-085
 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 B617 1 1 Nov 01/04R 1 1 1CES 1


 TASK 57-53-00-220-017
 Special Detailed Inspection of Outboard Double Slotted Flap, Tab Articulation at Stations 3A, 3B, 3C, 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


 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 
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