-
FOR 6084CM
panels 622FB, 622HB, 622JB, 622KB.

 (3)
 Make sure that the slats are retracted fully (Ref. TASK 27-80-00-866-005).

 (4)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on panel 114VU.

 (5) 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 removed component - on the torque shaft, outboard of the removed component.
 Subtask 27-84-45-865-091
 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 27-84-45-420-085 
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 27-84-45-420-086 
R  B. Installation of the Torque Shaft 6034CM(6084CM)
 (1) Install the universal joint (28).
 (2) Install the universal joint (35) and attach it with the pin (33) and the retaining ring (34).
 (3) Install the shaft (29) and attach it with the bolts (39) and the nuts (38).
 (4) Install the shaft (30) and attach it with the bolts (31) and (37) and the nuts (32) and (36).
 (5) TORQUE the nuts (32), (36) and (38) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
 (6) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (32), (36) and (38) - the bolts (31), (37) and (39) - the flanges of the universal joints (28) and (35) - the flanges of the shafts (29) and (30). 
R  (7) 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 removed components - from the torque shaft, outboard of the removed components.
 Subtask 27-84-45-210-076
R  C. Dimensional/Visual Checks (Ref. Fig. 402/TASK 27-84-45-991-002) 
R R R R R R (1) 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 27-84-45-865-092
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-45-710-057
 E. Test
 (1) Do an operational test of the slat power transmission system (Ref. TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
 5. Close-up
________ R (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-865-093
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 Subtask 27-84-45-410-059
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panels:

 -
FOR 6034CM
 install 522FB, 522HB, 522JB, 522KB

 -
FOR 6084CM
 install 622FB, 622HB, 622JB, 622KB.

 Subtask 27-84-45-865-094
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.

 Subtask 27-84-45-942-061
 D. Removal of Equipment
　
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8(15)