(a)
 Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines.

 - or

 (b)
 Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.

 1EFF : ALL 1 27-54-45Page A465 1 1 May 01/04R 1 1 1CES 1

 Subtask 27-54-45-420-062
 B. Installation of the Torque Shaft 6232CM(6282CM)
 (1)
 Install the universal joint (57) and align its flange with the flange of the steady bearing.

 (2)
 Install the torque shaft (58) and attach it with the bolts (60) and the nuts (59).

 (3)
 TORQUE the nuts (59) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).

 (4)
 Make sure that:

 -you cannot see the spline engagement groove at the movable joint
 -the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable joint.
 Subtask 27-54-45-916-060
 C. Application of Special Materials
 (1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
 -
the nuts (59)

 -
the bolts (60)

 -the flanges of the universal joint (57) and the torque shaft (58). R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-54-45-080-050
 D. Removal of Support Equipment
 (1) Remove the PIN RIGGING-FLAPS (TRACK 1) from the track 1 position. **ON A/C 301-399,
 Subtask 27-54-45-080-050-A
 D. Removal of Support Equipment
 (1) Remove the PIN RIGGING FLAPS from the track 1 position.

 **ON A/C ALL
 Subtask 27-54-45-865-098
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 27-54-45-710-062
 F. Operational Test of the Flap System
 (1)
 Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.

 (2)
 Do an operational test of the flap system (Ref. TASK 27-54-00-710-001). Make sure that the operation of the torque shafts is satisfactory.

 5. Close-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)
 **ON A/C ALL

 Subtask 27-54-45-410-060
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the COLLAR-SAFETY, SPOILER from the piston rod of the servo-control.

 (3)
 Put the applicable spoiler back to the 'O' (Operation) position (Ref. TASK 27-60-00-866-002).

 (4)
 On the servo-control, make sure that the pointer on the hex-head is opposite the letter 'O' (Operation) on the housing.

 (5)
 Install the applicable access panel (Ref. TASK 57-51-37-400-004):

 -
FOR 6232CM
 install 575FB, 575GB

 -
FOR 6282CM
 install 675FB, 675GB.

 Subtask 27-54-45-942-062
 B. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 CARRIAGE - REMOVAL/INSTALLATION
_______________________________
 TASK 27-54-46-000-002
 Removal of the No.1 Flap Carriage
 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 -------------------------------------------------------------------------------
　
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