TASK 27-54-45-000-007
 Removal of the Torque Shafts 6214CM(6264CM)/6220CM(6270CM)
 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.
 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 circuit breaker(s) safety clip(s) No specific safety barriers No specific warning sign No specific access platform 3.0 m (9 ft. 10 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 1EFF : ALL 1 27-54-45Page 479 1 1 May 01/00R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-50-00-866-008  Extension of the Flaps on the Ground
 27-54-44-000-002  Removal of the Steady Bearings FIN 6215CM(6265CM)/6219CM(6269CM)/6223CM (6273CM)/6225CM(6275CM)/6229CM(6279CM)/6231CM(6281CM)
 **ON A/C 001-049, 051-061, 101-103, 201-203,
 27-54-45-991-001 Fig. 401 R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 27-54-45-991-001-A  Fig. 401A
 **ON A/C 001-049, 051-061, 101-103, 201-203,
 27-54-45-991-003 Fig. 404 R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 27-54-45-991-003-A  Fig. 404A
 **ON A/C ALL
 3. Job Set-up
__________
 **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)R **ON A/C ALL

 Subtask 27-54-45-941-075
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning sign in position to tell persons not to operate the flap/slat controls.

 Subtask 27-54-45-860-056
 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 27-54-45-865-103
 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 27-54-45-010-055
 D. Get Access
 (1)
 Put the access platform in the applicable position.

 (2)
 Remove the applicable access panel:

 -
FOR 6214CM
 remove 573BB

 -
FOR 6220CM
 remove 575BB

 -
FOR 6264CM

 remove 673BB

 -
FOR 6270CM
 remove 675BB.

 (3)
 Remove the applicable steady bearing (56) (Ref. TASK 27-54-44-000-002):

 -
FOR 6214CM
 remove the steady bearing 6215CM

 -
FOR 6220CM
 remove the steady bearing 6219CM

 -
FOR 6264CM
 remove the steady bearing 6265CM

 -
FOR 6270CM
 remove the steady bearing 6269CM.

 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-103, 201-203,
　
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