(2)
Put a warning notice in position to tell persons not to operate the flap/slat controls.
Subtask 27-54-45-860-057
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever.
Subtask 27-54-45-865-055
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 27-54-45-010-056
D. Get Access
(1)
Put the access platform in the applicable position.
(2)
Remove the applicable access panel:
-
FOR 6216CM
remove 573CB (Ref. TASK 57-51-37-000-002)
-
FOR 6226CM
remove 575DB (Ref. TASK 57-51-37-000-004)
-
FOR 6266CM
remove 673CB (Ref. TASK 57-51-37-000-002)
-
FOR 6276CM remove 675DB (Ref. TASK 57-51-37-000-004).
(3)
Put the applicable spoiler in the 'M' (Maintenance) position (Ref. TASK 27-60-00-866-002).
(4)
Put the COLLAR-SAFETY, SPOILER on the piston rod of the servo-control.
4. Procedure
_________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 401/TASK 27-54-45-991-001)
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-54-45-991-001-A)
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 404/TASK 27-54-45-991-003) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 404A/TASK 27-54-45-991-003-A)
**ON A/C ALL
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.
**ON A/C 001-049, 051-061, 101-103, 201-203,
Subtask 27-54-45-020-057
A. Removal of the Torque Shafts 6216CM(6266CM and 6226CM(6276CM)
(1)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) to a flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the component to be removed.
(2)
Remove the nuts (59), the bolts (60) and the torque shaft (58).
(3) Remove the universal joint (57). R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
Subtask 27-54-45-020-057-A
A. Removal of the Torque Shafts 6216CM(6266CM and 6226CM(6276CM)
(1)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) to a flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the component to be removed.
(2)
Remove the nuts (59), the bolts (60) and the torque shaft (58).
(3)
Remove the plunging joint (57).
INTENTIONALLY BLANK
R 1 1
27-54-45Page 496
1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
TASK 27-54-45-400-008 Installation of the Torque Shafts 6216CM(6266CM)/6226CM(6276CM) WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(43)
