A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(178)

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R  (r) TORQUE the nut (39) to between 1.4 and 1.5 m.daN (10.32 and 11.06 
R  lbf.ft). 
R  (s) Manually operate the lever (28) and make sure that it moves 
R  freely. 
R  (t) Safety the nut (39) with the new cotter pin (38). 
R  (u) Remove the adjustable strut. 
R  (2) At the track 1 position: 
R  (Ref. Fig. 401B/TASK 27-54-55-991-001-C) 
R  (a) Connect the lever (10) to the flap link arm (5) as follows: 
R  1 Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (6)_ 
R  and the nut (8). 
R  (b) Install the bolt (6), the washer (7) and the nut (8). 
R  (3) At the track 2 position: 
R  (a) Connect the lever (28) to the flap link arm (32) as follows: 
R  1 Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (33)_ 
R  and to the nut (31). 
R  2 Install the bolt (33), the washer (29) and the nut (31)._ 
R  (4) Do a check of the flap rigged position (Ref. TASK 27-51-00-820-003). 
R  (5) At the track 1 position: 
R  (a) TORQUE the nut (8) to between 7.6 and 8.5 m.daN (56.04 and 62.68 
R  lbf.ft) and safety with a new cotter pin (9). 
R  (6) At the track 2 position: 
R  (a) TORQUE the nut (31) to between 1.8 and 2.2 m.daN (13.27 and 16.22 
R  lbf.ft) and safety with a new cotter-pin (30). 
R  (7) At tracks 1 and 2: 
R  (a) Apply STORAGE PRESERVATION (Material No. 15-007) to the bolts (6) 
R  and (33) and the nuts (8) and (31) after assembly. 

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R  (8) Install the Flap Track 2 Actuator 6211CM(6261CM) (Ref. TASK 27-54-49-
R  400-002). 
R  (9) Remove the locking tools LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH 
R  CLAMP-PIVOT from the torque shaft outboard of the track 2 actuator 
R  (Ref. TASK 27-50-00-000-003). 
R  (10) Remove the hoisting sling (Ref. TASK 27-50-00-000-002). 
R  **ON A/C 159-199, 211-212, 
R  Subtask 27-54-55-420-053-C 
R  B. Installation of the Flap-Actuator Lever Assembly - Track 1 
R  WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL_______ 
R  MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. 
R  OBEY THE MANUFACTURERS INSTRUCTIONS. 
R  PUT ON PROTECTIVE CLOTHING. 
R  DO NOT GET THEM IN YOUR MOUTH. 
R  DO NOT SMOKE. 
R  DO NOT BREATHE THE GAS. 
R  THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. 
R  GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 
R  (1) At the track 1 position: 
R  (Ref. Fig. 401B/TASK 27-54-55-991-001-C) 
R  (a) Apply COMMON GREASE (Material No. 04-022) to the bearing surfaces 
R  of the actuator lever (10). 
R  (b) Install the actuator lever (10) into the No.1 flap track beam. 
R  (c) Connect the No.1 flap track beam to the aircraft structure at the 
R  forward and the rear mountings (Ref. TASK 57-51-33-400-001). 
R  (d) Apply a layer of SPECIAL MATERIALS (Material No. 05-002) to the 
R  thread of the nuts (11). 
R  (e) Install the cover shell (1) with the bolts (2), (3) and (4) and 
R  the nuts (11). 
R  (f) TORQUE the bolts (2), (3) and (4) to between 1.4 and 1.6 m.daN 
R  (10.32 and 11.79 lbf.ft). 
R  (g) Remove the adjustable strut. 

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R  (h) Connect the lever (10) to the flap link arm (5) as follows: 
R  1_  Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (6)
R  and to the nut (8). 
R  2_  Install the bolt (6), the washer (7) and the nut (8).
R  (2) At the track 2 position: 
R  (Ref. Fig. 402/TASK 27-54-55-991-004) 
R  (a) Connect the lever (28) to the flap link arm (32) as follows: 
R  1_  Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (33)
R  and to the nut (31). 
R  2_  Install the bolt (33), the washer (29) and the nut (31).
R  (3) Do a check of the flap rigged position (Ref. TASK 27-51-00-820-003). 
R  (4) At the track 1 position: 
R  (a) TORQUE the nut (8) to between 7.6 and 8.5 m.daN (56.04 and 62.68 
　
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