(2)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed on the flap/slat control lever on panel 114VU.

R  (3) Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.
 (4) Make sure that the applicable steady bearing (15) is removed (Ref. TASK 27-84-44-000-001).
 (5) Make sure that the applicable access panel 191BB, 192FB is removed (Ref. TASK 53-35-13-000-002).
 Subtask 27-84-45-865-063
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 4. Procedure_________ 
R R (Ref. Fig. 402/TASK 27-84-45-991-002) 
Subtask 27-84-45-420-068 
R  A. Preparation for Installation 
R R  CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______ GREASE AND ASSEMBLY PASTE DO NOT MIX.
R R  (1) Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
 (2) Do an inspection of the component interface and/or the adjacent area.
 (3) Make sure that the parts retained from the removed component are clean and in the correct condition. 
R  (4) Do one of the steps that follow: 
R R  CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______ GREASE AND ASSEMBLY PASTE DO NOT MIX.

R R R R  (a) Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines. - or 
R R R (b) Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines. 
Subtask 27-84-45-420-069 
R  B. Installation of the Torque Shaft 6008CM(6058CM) 
R  (1) Put the retaining ring (18) in position over the shaft (14).
 (2) Install the universal joint (13) and attach it with the pin (12) and the retaining ring (18).
 (3) Install the shaft (14) and attach it with the bolts (17) and the nuts (16).
 (4) TORQUE the nuts (16) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
 (5) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (16) - the bolts (17) - the flange of the universal joint (13) - the flange of the shaft (14).
R R  (6) Install the applicable steady bearing (15) (Ref. TASK 27-84-44-400-001): - FOR 6008CM install the steady bearing 6007CM - FOR 6058CM install the steady bearing 6057CM.
R R R  (7) 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. 
R  (8) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003): - from the torque shaft inboard of the applicable component - from the torque shaft outboard of the applicable component.

 Subtask 27-84-45-865-098
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-45-710-058
 D. Test
R (1) The operational test of the slat power-transmission system is R contained in the installation of the steady bearing (Ref. TASK 27-84-44-400-001).
 5. Close-up
________ R Subtask 27-84-45-410-060
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Install the access panels 191BB, 192FB (Ref. TASK 53-35-13-400-002). Subtask 27-84-45-942-052
 B. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 TASK 27-84-45-000-004
R Removal of the Torque Shaft 6010CM(6060CM)
 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.

 1. Reason for the Job
__________________
　
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7(133)