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 m.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)