(Ref. Fig. 406A/TASK 57-55-11-991-007-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-55-11-010-052
 A. Lowering of the Flap Track Fairing
 (1)
 Remove the screws (2) and the top cover (1).

 (2)
 Remove the bolt (9), the washer (10) and disconnect the end of the bonding strap (8).

 (3)
 Remove and discard the cotter pin (6).

 (4)
 Disconnect the flap track fairing: WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME

_______ DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
 NOTE : The weight of the flap fairings is approximately 18kg (40lb).
____
 (a) Hold the movable fairing and remove the nut (3), the washer (4), the sliding bush (5) and the bolt (11).

 Flap No. 2 Movable Fairing - Location and Detail
 Figure 406/TASK 57-55-11-991-007

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-11Page 427 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Flap No. 2 Movable Fairing - Location and Detail R Figure 406A/TASK 57-55-11-991-007-A

R 1EFF : 301-399, 1 57-55-11Page 428 1 1 May 01/04 1 1 1CES 1

 (5) Lower the flap track fairing: CAUTION : MOVE THE MOVABLE FAIRING SLOWLY. DO NOT LET THE MOVABLE
_______ FAIRING TURN TOO FAR VERTICALLY BECAUSE THIS WILL CAUSE DAMAGE.
 (a) Carefully lower the movable fairing and make sure that the stops in the side load-stay hinge are engaged.
 **ON A/C 301-399,
 Subtask 57-55-11-010-052-A
 A. Lowering of the Flap Track Fairing
 (1)
 Remove the screws (2) and the cover (1).

 (2)
 Remove the nut (3), the bolt (6) and the washer (7). Disconnect the end of the bonding strap (4).

 (3)
 At the fairing drive link (5), disconnect the electrical harnesses

 (15) from the interface connector (14).

 (4)
 Remove and discard the lockwire and the cotter pin (10) from the applicable nuts (12) and (11).

 (5)
 Remove the nut (11) and the bolt (9).

 (6)
 Lower the fairing: WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME

_______ DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
 NOTE : The weight of the flap fairing assembly is approximately 18 kg
____
 (40 lb).

 (a)
 Hold the movable fairing and remove the nut (12), the washer (13) and the bolt (8).

 (b)
 Carefully lower the movable fairing and make sure that the stops in the side load-stay hinge are engaged.

 1EFF : ALL 1 57-55-11Page 429 1 1 May 01/05R 1 1 1CES 1

R **ON A/C ALL

 TASK 57-55-11-410-001
 To Lift the Flap Track No. 2 Movable Fairing after Access
 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.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific warning notices
 No specific access platform 3 m (9 ft. 10 in.)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-064 GB ABP1-4053 RELEASE AGENT (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (Ref. 20-31-00)
 Material No. 09-018  USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00) -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

Material No. 09-019  USA AMS 3267/3
 LOW ADHESION CORROSION INHIBITING SEALANT
 (Ref. 20-31-00)

 Material No. 11-004  USA MIL-T-81533
 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
 (Ref. 20-31-00)

 Material No. 19-003  USA AMS 3819
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼5(59)