(8)
 Install the bolt (1), the nut (6) and tighten it.

 (9)
 Safety the nut (6) with the cotter pin (7)

 (10) Put the bonding lead (17) in position, install the screw (16) and tighten it.
 NOTE : When you install the screw (16) do an electrical bonding of
____ the screw (Ref. TASK 20-28-00-912-004)
 (11) Put the bonding lead (8) in position, install the bolt (9), the nut
 (3) and tighten it.
 NOTE : When you install the bolt (9) do an electrical bonding of the

____
 bolt (Ref. TASK 20-28-00-912-004)

 Subtask 54-55-00-820-050
 B. Check and Adjustment of the Aft Movable Fairing R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 54-55-00-991-001)

 **ON A/C 301-399,

 (Ref. Fig. 401A/TASK 54-55-00-991-001-A) **ON A/C ALL
 (1) Make sure that the gap J1 between the inner flap and the movable fairing (19) of the pylon is 8 +3 -3 mm (0.3149 +0.1181 -0.1181 in.).
 NOTE : You must measure the gap J1 on the inboard and outboard sides
____
 of the movable fairing (19).

 (2) If necessary adjust it with the adjustable fitting (18) at the bottom of the rod.
 5. Close-up
________ Subtask 54-55-00-440-050
 A. Aircraft Maintenance Configuration
 (1)
 Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).

 (2)
 Set the flap/slat control lever to position 1 (Ref. TASK 27-50-00-866-008).

 Subtask 54-55-00-410-050
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access panels:

 (a)
 For the left pylon: 475CL, 476CR, 477AL

 (b)
 For the right pylon: 485CL, 486CR, 487AR

 (3)
 Remove the access platform(s).

 (4)
 Remove the warning notice(s).

 1EFF : ALL 1 54-55-00Page 410 1 1 May 01/05R 1 1 1CES 1

 AFT MOVABLE FAIRING - INSPECTION/CHECK
______________________________________
 TASK 54-55-00-200-001
 Inspection of the Aft Movable Fairing
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 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 notice
 No specific access platform 1.7 m (5 ft. 7 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
54-55-00-000-001 Removal of the Aft Movable Fairing 54-55-00-400-001 Installation of the Aft Movable 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 54-55-00-991-002 Fig. 601 54-55-00-991-003 Fig. 602

 3. Job Set-up
__________ Subtask 54-55-00-941-051
 A. Safety Precautions
 (1)
 On the center pedestal, on the ENG panel 115VU:

 (a) Put a warning notice to tell persons not to start the engine.

 (2)
 Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do this procedure.

 (3)
 On the overhead maintenance panel 50VU:

 (a)
 Make sure that the ON legend of the ENG/FADEC GND PWR/1 (2) pushbutton switch is off.

 (b)
 Put a warning notice to tell persons not to energize the FADEC 1(2)

 Subtask 54-55-00-040-051
 B. Aircraft Maintenance Configuration
 (1)
 Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 54-55-00-941-052

 C. Get Access
 (1) Put the access platform in position:
 (a) in the zone 470 for the left pylon,

 (b)
 in the zone 480 for the right pylon. Subtask 54-55-00-020-051

 D. Removal of Component
 (1) Remove the aft movable fairings (Ref. TASK 54-55-00-000-001).
　
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 NACELLES/PYLONS(101)