(3)
 Remove the warning notice(s).

 AFT MOVABLE FAIRING - DESCRIPTION AND OPERATION
_______________________________________________
 1. Description
___________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 001)
 **ON A/C 301-399,
 (Ref. Fig. 001A)
 **ON A/C ALL
 The movable fairing is hinged at RIB14 and linked to the flap by a rod
 attached to the fairing by a serrated plate system.
 The movable fairing is composed of:

 -
an inner structure made of stainless steel and titanium alloy.

 -
an outer skin made of carbon and honeycomb
 - one access panel.
 The access panels are bolted.
 Standard attachment is by aluminum alloy rivets

 Movable Fairing
 Figure 001

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 54-55-00Page 2 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  Movable Fairing 
R  Figure 001A
 1EFF :  301-399,  1  54-55-00 Page 3 
1  1  May 01/04
 1  1
 1CES  1

 AFT MOVABLE FAIRING - REMOVAL/INSTALLATION
__________________________________________
 TASK 54-55-00-000-001
 Removal 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 1.5 m (4 ft. 11 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-50-00-866-008  Extension of the Flaps on the Ground
 78-30-00-481-041  Make the Thrust Reverser Unserviceable for
 Maintenance

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 54-55-00-991-001 Fig. 401
 **ON A/C 301-399,

 54-55-00-991-001-A  Fig. 401AR **ON A/C ALL

 3. Job Set-up
__________
 Subtask 54-55-00-941-050

 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 54-55-00-040-050
 B. Aircraft Maintenance Configuration
 (1)
 Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).

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

 Subtask 54-55-00-010-050
 C. Get Access
 (1)
 Put an access platform in position

 (a)
 at the zone 470 for the left pylon

 (b)
 at the zone 480 for the right pylon

 (2)
 Remove the access panels:

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

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

 4. Procedure
_________
 Subtask 54-55-00-020-050

 A. Removal 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)
 Remove the nut (3), the screw (9) and release the bonding lead (8).
　
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