A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(177)_航空信息_民用航空_通用航空

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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.
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)._

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R (2) At the track 2 position:
R (Ref. Fig. 402A/TASK 27-54-55-991-004-B)
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
R lbf.ft) and safety with a new cotter pin (9).
R (5) 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 (6) 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.
R (7) Install the Flap Track 1 Actuator 6205CM(6255CM) (Ref. TASK 27-54-49-
R 400-001).
R Subtask 27-54-55-420-061-D
R C. Installation of the Flap-Actuator Lever Assembly - Track 2
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.

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R (1) At the track 2 position:
R (Ref. Fig. 402A/TASK 27-54-55-991-004-B)
R (a) Apply SEALANTS (Material No. 09-018) to the bolts (43).
R (b) Install the bolts (43) in the outboard bracket (36) with the bolt
R heads inboard.
R (c) Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No.
R 09-019) to the mating face of the anti-rotation plate (42).
R (d) Install the anti-rotation plate (42) on the bolts (43) and
R loosely install the nuts (41).
R (e) Apply SPECIAL MATERIALS (Material No. 05-064) to the holes of the
R bearing housings in the brackets (36).
R (f) Apply SEALANTS (Material No. 09-018) to the plain shank and
R flange of the bearing housing (34).
R (g) Install the bearing housing (34) in the outboard bracket (36) and
R tighten the nuts (41).
R (h) Apply COMMON GREASE (Material No. 04-022) to the ring nut (40).
R (i) Install the ring nut (40) on the bearing housing (34).
R (j) Torque the ring nut (40) with the SPANNER-FLAP LEVER TRACKS 2 AND
R 3 (98D27504028000) to between 1.4 and 1.5 m.daN (10.32 and 11.06
R lbf.ft).
R (k) If necessary, drill a 2.5 mm (0.10 in.) hole for the cotter pin
R (37) in an applicable position on the bearing housing (34).
R Remove all unwanted material from the area.
R (l) Safety the ring nut (40) with a new cotter-pin (37).
R (m) Apply COMMON GREASE (Material No. 04-022) to the bearing surfaces
R of the lever (28).
R (n) Turn the lever (28) through 90 deg. and install it in the bearing
R housing (34).
R (o) Install the bearing housing (26), the bolt (25) and the nut (44).
R (p) Apply COMMON GREASE (Material No. 04-022) to the retention plate
R (35) and to the bolt (27).