(5)
 TORQUE the nuts (4) and (8) to between 1.02 and 1.24 m.daN (90.26 and

 109.73 lbf.in).

 (6)
 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.

 (7)
 Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003).

 Subtask 27-54-45-916-054
 C. Application of Special Materials
 (1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
 -
the nuts (4) and (8)

 -
the bolts (3) and (9)

 -
the flanges of the universal joints (1) and (7)

 -the flanges of the torque shaft (2).
 Subtask 27-54-45-865-072

 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 27-54-45-710-054
 E. Operational Test of the Flap System
 (1)
 Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.

 (2)
 Retract the flaps fully (Ref. TASK 27-50-00-866-009).

 (3)
 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
________ R **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 27-54-45-410-054
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panel (Ref. TASK 57-51-37-400-002):

 -
FOR 6210CM
 install 573AB

 -
FOR 6260CM
 install 673AB.

 Subtask 27-54-45-942-054
 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.

 TASK 27-54-45-000-006
 Removal of the Torque Shaft 6212CM(6262CM)
 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.) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 1EFF : ALL 1 27-54-45Page 466 1 1 May 01/00R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001)
 27-50-00-866-008 Extension of the Flaps on the Ground
 27-54-45-000-007 Removal of the Torque Shafts

 6214CM(6264CM)/6220CM(6270CM)
 57-51-37-000-002 Removal of the Access Panels 573AB(673AB),
 573BB(673BB), 573CB(673CB)

 **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,
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(35)