____
(2)
At the forward mounting:
(a)
Remove the nut (13) from the bolt (12).
(b)
Remove the bolt (12) and the bush (11) from the bracket (14).
(3)
At the rear mounting:
(a)
Remove the nuts (6), the bolts (5) and the bushes (4).
(b)
Remove the nut (8) and the bush (7) from the bolt (2).
(c)
Remove the bolt (2) and the bush (3) from the bracket (10).
(d)
Lower the flap track beam (1) and remove the ball pin (9).
(4) Remove the flap track beam (1).
**ON A/C 301-399,
Subtask 57-51-33-020-053-B
A. Removal of the Flap Track Beam WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME DAMAGED OR
_______
INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
(1) Hold the flap track beam (1). NOTE : The weight of the flap track beam (1) is 28 kg (61.7294 lb).
____
R 1EFF : 062-099, 104-149, 151-199, 204-299, 1 57-51-33Page 409 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
R (2) At the front mounting:
R (a) Release the lockwasher (15) and remove the nut (16).
R (b) Remove and discard the lockwasher (15).
R (c) Remove the bolt (11).
R (d) Remove and discard the lockwire and remove the nut (14).
R (e) Remove the washer (13) and the hollow bolt (12).
R (3) At the rear mounting:
R (a) Remove and discard the cotter pin (2).
R (b) Remove the nut (3), the washer (4) and the bolt (10).
R (c) Release the lockwasher (6) and remove the nut (5).
R (d) Remove and discard the lockwasher (6).
R (e) Remove the washer (7).
R (f) Remove the hollow bolt (9) and the bush (8).
R (4) Remove the flap track beam (1).
R 1EFF : 301-399, 1 57-51-33Page 410 1 1 May 01/04 1 1 1CES 1 **ON A/C ALL
TASK 57-51-33-400-001
Installation of the No.1 Flap Track Beam
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notices
No specific access platform 3 m (9 ft. 10 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
(15.00 to 150.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 04-024
R
R
Material No. 05-002
Material No. 09-005
Material No. 09-013
Material No. 11-026
Material No. 15-004
Material No. 19-003
R Material No. 19-010
R
R
AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00)USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)USA MIL-PRF-81733 TYPE I CLASS A CORROSION INHIBITING BRUSH CONSISTENCY (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA MIL-C-16173 GRADE 3 CORROSION PREVENTIVE COMPOUND (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼3(137)
