-
dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 in.) along the full length of the panel. Try and set the clearance as near as possible to 2.0 mm (0.0787 in.).
-
dimension Y is between 3.0 mm (0.1181 in.) and 6.0 mm (0.2362 in.) along the full width of the panel outboard end. Try and set the clearance as near as possible to 4.0 mm (0.1574 in.).
(c)
Attach the access panel (2) to the wing with the remaining camloc fasteners (1).
(d)
Fill the clearance between the access panel (2) and the trailing edge of the wing skin with SEALANTS (Material No. 09-016).
5. Close-up
________
Subtask 57-51-37-942-055
A. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Remove the safety barriers.
(4)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (Ref. TASK 27-00-00-080-002) from the flap/slat control lever.
(5)
Remove the warning notice(s).
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TASK 57-51-37-000-003
Removal of the Access Panel 573FB(673FB)
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
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice
No specific adjustable access platform 4 m (13 ft. 1 in.)
98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking
Tool (98D27803000000) 27-50-00-866-009 Retraction of the Flaps on the Ground 57-51-37-991-004 Fig. 402
3. Job Set-up
__________
(Ref. Fig. 402/TASK 57-51-37-991-004)
Subtask 57-51-37-941-054
A. Safety Precautions
(1)
Put the warning notice in the cockpit to tell persons not to operate the flaps/slats.
(2)
Make sure that the flaps/slats are fully retracted (Ref. TASK 27-50-00-866-009) and install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) (Ref. TASK 27-00-00-480-002) on the flap/slat control lever. Put the safety barriers in position.
Subtask 57-51-37-010-053
B. Get Access
(1) Put the adjustable access platform below the applicable access panel, zone 573(673).
4. Procedure
_________
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.
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Lower Trailing Edge Access Panel 573FB(673FB) Figure 402/TASK 57-51-37-991-004
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Subtask 57-51-37-020-051
A. Removal of the Access Panel
(1) Remove the screws (1) then remove the access panel (2).
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TASK 57-51-37-400-003 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼3(163)
