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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