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时间:2011-03-27 12:43来源:蓝天飞行翻译 作者:航空
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 A. Remove the hinge pins
 (1) Remove the two applicable inner hinge pins:
 -
for the spoiler 1 (Ref. TASK 27-64-41-000-001)

 -
for the spoiler 2 (Ref. TASK 27-64-42-000-001)

 -
for the spoiler 3 (Ref. TASK 27-64-43-000-001)

 -
for the spoiler 4 (Ref. TASK 27-64-44-000-001)

 -
for the spoiler 5 (Ref. TASK 27-64-45-000-001).


 Subtask 57-51-00-110-089
 B. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the two inner hinge pins.


R  Spoiler Hinge Pins Figure 625/TASK 57-51-00-991-024
 1EFF : 1 1 1CES  ALL  1 111 57-51-00 Page A652 Nov 01/04

 

 Subtask 57-51-00-210-071
 C. Inspection
 (1) Examine the two inner hinge pins for:
 -corrosion
 -damage
 -scratches and/or scores
 -correct condition of the protective finish.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the

____
 correct repair procedure.

 Subtask 57-51-00-420-078
 D. Install the Hinge Pin
 (1) Install the two applicable inner hinge pins:
 -
for the spoiler 1 (Ref. TASK 27-64-41-400-001)

 -
for the spoiler 2 (Ref. TASK 27-64-42-400-001)

 -
for the spoiler 3 (Ref. TASK 27-64-43-400-001)

 -
for the spoiler 4 (Ref. TASK 27-64-44-400-001)

 -
for the spoiler 5 (Ref. TASK 27-64-45-400-001).


 5. Close-up
________ Subtask 57-51-00-410-081
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the applicable access panels:


 -for the left wing, install 573CB, 575AB, 575DB, 575EB, 575GB
 -for the right wing, install 673CB, 675AB, 675DB, 675EB, 675GB. Subtask 57-51-00-942-079
 B. Removal of Equipment
 (1)
 Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).


R 1EFF : ALL 1 57-51-00Page A653 1 1 Nov 01/04 1 1 1CES 1


 (4)
 Remove the safety barriers.

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 1EFF : ALL 1 57-51-00Page A654 1 1 Nov 01/04R 1 1 1CES 1

 TASK 57-51-00-220-016


 Detailed Visual Inspection of Outer Wing Trailing Edge Aileron Hinge Pins 1 thru 5
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 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.
 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.
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 575120-03
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific slave bolts No specific warning notices No specific access platform 3 m (9 ft. 10 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 1EFF : ALL 1 57-51-00Page A655 1 1 Nov 01/04R 1 1 1CES 1


 -------------------------------------------------------------------------------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)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
 
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