A320飞机维护手册 AMM WINGS 机翼3(125)

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R  (12) Sufficiently support the shroud box. 
R  NOTE : The weight of the shroud box is approximately 30 kg (66.1386____ 
R  lb). 
R  (13) At the outboard forward attachment bracket: 
R  (a) Remove the nut (83), the bolt (85) and disconnect the bonding 
R  strap (82) from the tag (84). 
R  (b) Remove the cotter-pin (80), the nut (79), the washer (81), the 
R  bolt (75) and the washer (76). 
R  (c) Remove the slider bushes (77) from the outboard forward 
R  attachment bracket (78). 
R  (d) Discard the cotter-pin (80). 
R  (14) At the outboard aft attachment bracket: 
R  (a) Remove the nut (95), the bolt (97) and disconnect the bonding 
R  strap (94) from the tag (96). 
R  (b) Remove the cotter-pin (98), the nut (88), the washer (89), the 
R  bolt (92) and the washer (93). 
R  (c) Remove the floating bushes (90) from the outboard aft attachment 
R  bracket (91). 
R  (d) Discard the cotter-pin (98). 
R  (15) At the inboard aft attachment bracket: 
R  (a) Remove the nut (52), the bolt (50) and disconnect the bonding 
R  strap (55) from the bracket (51). 
R  (b) Remove the cotter-pin (59), the nut (60), the washer(s) (58), the 
R  bolt (53) and the washer (54). 
R  (c) Remove the floating bush (57) from the inboard aft attachment 
R  bracket (61). 

R 1EFF : 401-499, 1 57-51-15Page 417 1 1 Aug 01/05 1 1 1CES 1

R  (d) Discard the cotter-pin (59). 
R  (e) Move the end of the rod (56) clear of the inboard aft attachment 
R  bracket (61). Do not adjust the length of the rod (56). The rod 
R  (56) is set and locked at aircraft build and must not be 
R  adjusted. 
R  (16) At the inboard center attachment bracket: 
R  (a) Remove the cotter-pin (43), the nut (44), the washer(s) (45), the 
R  bolt (40) and the washer (41). 
R  (b) Remove the floating bush (46) from the inboard center attachment 
R  bracket (42). 
R  (c) Discard the cotter-pin (43). 
R  (d) Move the end of the rod (47) clear of the inboard center 
R  attachment bracket (42). Do not adjust the length of the rod 
R  (47). The rod (47) is set and locked at aircraft build and must 
R  not be adjusted. 
R  (17) At the inboard forward attachment bracket: 
R  (a) Remove the nut (28), the bolt (34) and disconnect the bonding 
R  strap (33) from the bracket (27). 
R  (b) Remove the cotter-pin (29), the nut (30), the washer(s) (31), the 
R  bolt (24) and the washer (25). 
R  (c) Remove the floating bush (32) from the inboard forward attachment 
R  bracket (26). 
R  (d) Discard the cotter-pin (29). 
R  (e) Move the end of the rod (35) clear of the inboard forward 
R  attachment bracket (26). Do not adjust the length of the rod 
R  (35). The rod (35) is set and locked at aircraft build and must 
R  not be adjusted. 
R  (18) To remove the shroud box from the wing: 
R  (a) Carefully break the bond of the sealant between the shroud box 
R  and the overwing panel. 

R 1EFF : 401-499, 1 57-51-15Page 418 1 1 Aug 01/05 1 1 1CES 1R (b) Carefully disengage the outboard attachment brackets on the R shroud box from the related brackets on the fixed shroud. Lower R the shroud box clear of the aircraft and put it on a clean R surface.

R 1EFF : 401-499, 1 57-51-15Page 419 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL

 TASK 57-51-15-400-001
 Installation of the Shroud Box 572(672)
 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.

 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
　
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