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时间:2011-03-27 08:52来源:蓝天飞行翻译 作者:admin
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R  (2) Connect the two drain lines (21) and (22). 
R  5. Close-up________ 
R  Subtask 54-54-00-420-056 
R  A. Installation of the Fairings 
R  (1) Install the lower fairing (Ref. TASK 54-56-00-400-001). 
R  (2) Install the aft movable fairing (Ref. TASK 54-55-00-400-001). 
R  Subtask 54-54-00-440-052 
R  B. Aircraft Maintenance Configuration 
R  (1) Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).

 

R Subtask 54-54-00-410-052

R  C. Close Access 
R  (1) Install these access panels: 
R  (a) for the left pylon: 471CL, 475BL, 476BR. 
R  (b) for the right pylon: 482CR, 486BR, 485BL. 
R  (2) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (3) Remove the access platform(s). 
R  (4) Remove the warning notice(s).

 

 AFT FIXED FAIRING - INSPECTION/CHECK
____________________________________
 TASK 54-54-00-200-001
 Inspection of the Aft Fixed 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 1.8 m (5 ft. 11 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
54-54-00-000-001 Removal of the Aft Fixed Fairing 54-54-00-400-001 Installation of the Aft Fixed 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 54-54-00-991-003 Fig. 601 54-54-00-991-004 Fig. 602 54-54-00-991-005 Fig. 603 54-54-00-991-006 Fig. 604

 3. Job Set-up
__________

 Subtask 54-54-00-941-052
 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 54-54-00-040-050
 B. Aircraft Maintenance Configuration
 (1)
 Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 54-54-00-941-053

 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 54-54-00-020-051


 D. Removal of Component
 (1) Remove the aft fixed fairing (Ref. TASK 54-54-00-000-001).


 4. Procedure
_________
 (Ref. Fig. 601/TASK 54-54-00-991-003, 602/TASK 54-54-00-991-004, 603/TASK
 54-54-00-991-005, 604/TASK 54-54-00-991-006)
 Subtask 54-54-00-220-050
 A. Inspection of the Aft Fixed Fairing
 (Ref. Fig. 602/TASK 54-54-00-991-004)

 (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
 -------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)| |--------|---------|---------|---------|---------|---------|---------|--------| | E | 0.3740 | 0.3745 | | | 0.3733 | | | | OD 1 | (9.499) | (9.512) | | | (9.481) | | | | | | | 0.0003 | 0.0014 | | | 0.0028| | | | | (0.007) | (0.035) | | |(0.071) | | E | 0.3748 | 0.3754 | | | | 0.3761 | | | ID 2 | (9.519) | (9.535) | | | | (9.552) | | -------------------------------------------------------------------------------
 
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