A320飞机维护手册 AMM WINGS 机翼5(73)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  (i) Put the rear fairing (1) in position and loosely install the 
R  screws (2). 
R  (j) Adjust the rear fairing (1) until the dimension X is 5 +3 -1 mm 
R  (0.2 +0.12 -0.04 in). 
R  (k) Tighten the screws (2) and TORQUE to between 0.7 and 0.8 m.daN 
R  (61.94 and 70.79 lbf.in). 
R  (l) Apply a bead of SEALANTS (Material No. 09-016) between the tab 
R  trailing edge and the rear fairing (1). 
R  (2) Install the inboard flap tab-fairings at the hinge 1B position as 
R  follows: 
R  (Ref. Fig. 414/TASK 57-55-11-991-018) 
R  (a) Hold the front fairing (29) and connect the bonding strap (39) 
R  with (Ref. TASK 20-28-00-912-004): 
R  - the bolt (41) 
R  - the washers (40) and (38) 
R  - the nut (37). 
R  (b) TORQUE the nut (37) to between 0.35 and 0.45 m.daN (30.97 and 
R  39.82 lbf.in). 
R  (c) Engage the front fairing (29) on the bolts (36) and carefully 
R  push the front fairing (29) into position. 
R  (d) Install the washers (28) and (32) and the bolts (27) and (31). 
R  (e) TORQUE the bolts (27) and (31) to between 1.4 and 1.6 m.daN 
R  (10.32 and 11.79 lbf.ft).

 

R  (f) Install the caps (26) and (30). 
R  (g) Hold the rear fairing (22) and connect the bonding strap (39) 
R  with (Ref. TASK 20-28-00-912-004): 
R  - the bolt (41) 
R  - the washers (40) and (38) 
R  - the nut (37). 
R  (h) TORQUE the nut (37) to between 0.35 and 0.45 m.daN (30.97 and 
R  39.82 lbf.in). 
R  (i) Engage the rear fairing (22) on the screws (21) and carefully 
R  push the rear fairing (22) into position. 
R  (j) Adjust the rear fairing (22) until the dimension Y is 5 +3 -1 mm 
R  (0.2 +0.12 -0.04 in). 
R  (k) Tighten the screws (21) and TORQUE to between 0.7 and 0.8 m.daN 
R  (61.94 and 70.79 lbf.in). 
R  (l) Install the washers (25) and (35) and the bolts (24) and (34). 
R  (m) Install the caps (23) and (33). 
R  (n) Apply a bead of SEALANTS (Material No. 09-016) between the tab 
R  trailing edge and the rear fairing (22). 
R  (3) Install the outboard flap tab-fairings at the hinge 3A, 3B and 3C 
R  positions as follows: 
R  (Ref. Fig. 415/TASK 57-55-11-991-017) 
R  NOTE : The installation of the hinge 3A, 3B and 3C fairings is almost____ 
R  the same. 
R  (a) Put the front fairing (61) in position and install the screws 
R  (55). 
R  (b) Tighten the screws (55). 
R  (c) Hold the rear fairing (53) and connect the bonding strap (66) 
R  with (Ref. TASK 20-28-00-912-004): 
R  - the bolt (68) 
R  - the washers (67) and (65) 
R  - the nut (64). 
R  (d) Put the rear fairing (53) in position and loosely install the 
R  screws (52) and (54).

 

R R  (e) Adjust the rear fairing (53) until the dimension Z is 5 +3 -1 mm (0.2 +0.12 -0.04 in). 
R  (f) Tighten the screws (52) and (54). 
R R  (g) Apply a bead of SEALANTS (Material No. 09-016) between the tab trailing edge and the rear fairing (53).
 Subtask 57-55-11-865-065
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 57-55-11-860-056
 D. Aircraft Configuration
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control-lever.
 Subtask 57-55-11-710-056
 E. Test 
R R  (1) Do an operational test of the flap system (Ref. TASK 27-54-00-710-001) to make sure that the hinge fairings operate correctly.
 5. Close-up________
 Subtask 57-55-11-942-058
 A. Removal of Equipment
 (1) Remove the access platform(s).
 (2) Remove the warning notice(s).
 (3) Remove the safety barriers.
 (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 

 TASK 57-55-11-000-006
 Removal of the Hinge 1A Extension Fairing
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:
　
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