R 3. Job Set-up
__________
R Subtask 57-55-11-941-071
R A. Safety Precautions
R (1) Put warning notices in the cockpit to tell persons not to operate the
R flaps or slats.
R (2) Put the safety barriers in position.
R Subtask 57-55-11-860-073
R B. Aircraft Maintenance Configuration
R (1) Make sure that the flaps are in the fully retracted position
R (Ref. TASK 27-50-00-866-009).
R (2) Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001)
R on the flap/slat control-lever.
R Subtask 57-55-11-865-077
R C. Open, safety and tag this(these) circuit breaker(s):
R -------------------------------------------------------------------------------
R PANEL DESIGNATION IDENT. LOCATION
R -------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07
R 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
R Subtask 57-55-11-010-059
R D. Get Access
R (1) Put the adjustable access platform below the fairing at flap track 2,
R zone 531 (631).
R (2) Remove the flap track 2 fixed fairing 531EB (631EB) (Ref. TASK 57-55-
R 11-000-004).
R 4. Procedure
_________
R (Ref. Fig. 417/TASK 57-55-11-991-025)
R Subtask 57-55-11-020-075
R A. Removal of the Flap Track 2 Fairing Bracket and Link Assembly
R NOTE : When you remove the bracket and link assembly from the wing, make____
R sure you do not move the bracket attachment bolts.
R (1) Remove the nuts (8).
R (2) Carefully remove the bracket (1) and link assembly (4) from the wing.
R (3) Disassemble the bracket and link assembly as follows:
R (a) Remove and discard the cotter pin (7).
R (b) Remove the nut (6), the washer (5) and the bolt (3).
R (c) Slide out the sleeve (2) and separate the bracket (1) from the
R link assembly (4).
R Flap Track 2 Fairing Bracket and Link Assembly - Location and Detail R Figure 417/TASK 57-55-11-991-025
1EFF : 301-399, 1 57-55-11Page 498 1 1 Aug 01/04 1 1 1CES 1
TASK 57-55-11-400-007
Installation of the Flap Track 2 Fairing Bracket and Link Assembly
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 warning notices R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 09-002 USA MIL-S-8802 TYPE I CLASS B
FUEL TANK SEALANTPOLYSULFID(NO LONGER AVAILABLE
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
cotter pin 57-55-05 20D-100
R D. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
中國航空網 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(77)
