(1)
 Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). Subtask 54-54-00-865-054

 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2701GJ, 2702GJ, 3801GX, 3802GX, 3803GX

 Subtask 54-54-00-410-050

 D. Close Access
 (1)
 Install these access panels:

 (a)
 for the left pylon: 471CL, 475BL, 476BR.

 (b)
 for the right pylon: 482CR, 486BR, 485BL.

 (2)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (3)
 Remove the access platform(s).

 (4)
 Remove the warning notice(s).

 TASK 54-54-00-400-001- 01

 Installation of the Aft Fixed Fairing
 1. Reason for the Job
__________________
 This is an alternative method without installation of the hydraulic lines.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
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)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
54-55-00-400-001 Installation of the Aft Movable Fairing
 54-56-00-400-001 Installation of the Lower Fairing
 78-30-00-081-041 Make the Thrust Reverser Serviceable after

 Maintenance
 78-30-00-481-041 Make the Thrust Reverser Unserviceable for

 Maintenance
 54-54-00-991-009 Fig. 403
 54-54-00-991-007 Fig. 404
 54-54-00-991-008 Fig. 405

R  3. Job Set-up__________ 
R  Subtask 54-54-00-860-052 
R  A. Aircraft Maintenance Configuration 
R  (1) Make sure that the access platform is in position. 
R  (2) Make sure that the warning notices are in position. 
R  (3) Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). 
R  4. Procedure_________ 
R  Subtask 54-54-00-420-055 
R  A. Installation of the Aft Fixed Fairing 
R  (Ref. Fig. 405/TASK 54-54-00-991-008) 
R  (1) Put the aft fixed fairing in position. 
R  NOTE : Two persons are necessary to move the aft fixed fairing.____ 
R  (2) Install the bolts (9) and the nuts (10), (7) and (8). 
R  (3) Install the washer (12), the bolt (14), the washer (15) and the nut 
R  (16). 
R  (4) Install the bolt (11) and the nut (13). 
R  (5) TORQUE the nuts (10) and (7) to between 2.6 and 3 m.daN (19.17 and 
R  22.12 lbf.ft). 
R  (6) TORQUE the nut (8) to between 0.35 and 0.45 m.daN (30.97 and 39.82 
R  lbf.in). 
R  (7) TORQUE the nut (16) to between 3.6 and 4.1 m.daN (26.54 and 30.23 
R  lbf.ft). 
R  (8) TORQUE the nut (13) to 1.5 m.daN (11.06 lbf.ft). 
R  (9) Put the bonding lead (19) in position. 
R  (10) Install the washer (18). Install the screw (17) and tighten it. 
R  NOTE : Do an electrical bonding of the screw (17) when you install it____ 
R  (Ref. TASK 20-28-00-912-004).

R Subtask 54-54-00-420-058

R  B. Installation of the Fitting and the Plate 
R  (Ref. Fig. 404/TASK 54-54-00-991-007) 
R  (1) Put the fitting (4) in position. 
R  (2) Install the bolts (5) and the nuts (3). 
R  (3) Tighten the nuts (3). 
R  (4) Put the plate (6) in position. 
R  (5) Install the bolts (1) and the nuts (2). 
R  (6) Tighten the nuts (2). 
R  Subtask 54-54-00-420-059 
R  C. Connection of the Drain Lines 
R  (Ref. Fig. 403/TASK 54-54-00-991-009) 
R  (1) Remove the blanking plugs from the disconnected line ends. 
　
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 NACELLES/PYLONS(93)