A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(15)

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 (1) Put the safety barriers in position.
 (2) Put a warning notice in the cockpit to tell persons not to operate the landing-gear doors.
 (3) Put a warning notice on panel 114VU to tell persons not to operate the flap/slat controls.
 Subtask 27-54-44-865-056
 B. 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 27-54-44-860-051
 C. 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)
 Retract the flaps fully (Ref. TASK 27-50-00-866-009).

 (2)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever on panel 114VU.

 Subtask 27-54-44-010-050
 D. Get Access
R (1) Put the access platform in position below the applicable torque R shaft.
 (2) Remove the applicable torque shaft (11) (Ref. TASK 27-54-45-000-008), (Ref. TASK 27-54-45-000-009), (Ref. TASK 27-54-45-000-010), (Ref. TASK 27-54-45-000-012), (Ref. TASK 27-54-45-000-013):
 -
FOR 6215CM
 remove the torque shaft 6216CM

 -
FOR 6225CM
 remove the torque shaft 6226CM

 -
FOR 6265CM
 remove the torque shaft 6266CM

 -
FOR 6275CM
 remove the torque shaft 6276CM

 -
FOR 6219CM
 remove the torque shaft 6218CM

 -
FOR 6269CM
 remove the torque shaft 6268CM

 -
FOR 6223CM
 remove the torque shaft 6222CM

 -
FOR 6273CM
 remove the torque shaft 6272CM

 -
FOR 6229CM
 remove the torque shaft 6228CM

 -
FOR 6279CM
 remove the torque shaft 6278CM

 -
FOR 6231CM
 remove the torque shaft 6232CM

 -
FOR 6281CM
 remove the torque shaft 6282CM.

 

 

R (3) For steady bearings FIN 6231CM (6281CM), remove the applicable access R panel (Ref. TASK 57-51-37-000-004):
 -
FOR 6231CM
 remove 575EB

 -
FOR 6281CM
 remove 675EB.

 

 (4) Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-54-44-991-001)
 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 27-54-44-020-051
 A. Removal of the Steady Bearing Assemblies
 (1) Remove the nuts (13), the bolts (12) and the steady bearing (16).

 TASK 27-54-44-400-002
 Installation of the Steady Bearings FIN 6215CM(6265CM)/6219CM(6269CM)/6223CM (6273CM)/6225CM(6275CM)/6229CM(6279CM)/6231CM(6281CM) 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 -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice
 No specific access platform 2.5 m (8 ft. 2 in.)
　
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