-------------------------------------------------------------------------------| 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)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 0.4364 | 0.4369 | | | 0.4348 | | | | OD 10 |(11.084) |(11.097) | | |(11.043) | | | | | | | 0.0021 | 0.0033 | | | 0.0065| | | | | (0.053) | (0.083) | | |(0.165) | | F | 0.4390 | 0.4397 | | | | 0.4413 | | | ID 12 |(11.150) |(11.168) | | | |(11.209) | | -------------------------------------------------------------------------------
Subtask 54-55-00-220-058
R L. Inspection of the Aft Movable Fairing (Ref. Fig. 602/TASK 54-55-00-991-003)
(1) Measure these dimensions of the aft movable fairing and make sure that they 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)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 0.4364 | 0.4369 | | | 0.4348 | | | | OD 10 |(11.084) |(11.097) | | |(11.043) | | | | | | | 0.0021 | 0.0033 | | | 0.0065| | | | | (0.053) | (0.083) | | |(0.165) | | F | 0.4390 | 0.4397 | | | | 0.4413 | | | ID 11 |(11.150) |(11.168) | | | |(11.209) | | -------------------------------------------------------------------------------
5. Close-up
________ Subtask 54-55-00-420-051
A. Installation of Component Make sure that the work area is clean and clear of tool(s) and other items.
(1)
Install the aft movable fairings (Ref. TASK 54-55-00-400-001). Subtask 54-55-00-440-051
B. Aircraft Maintenance Configuration
(1)
Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). Subtask 54-55-00-942-051
C. Close Access
(1)
Remove the warning notice(s).
(2)
Remove the access platform(s).
SEAL - AFT MOVABLE FAIRING - REMOVAL/INSTALLATION_________________________________________________
TASK 54-55-41-000-001
Removal of the Aft Movable-Fairing Seals
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 -------------------------------------------------------------------------------
R R No specific No specific warning notice access platform 2 m (6 ft. 7 in.)
R B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R 27-50-00-866-008 78-30-00-481-041 54-55-41-991-001 Extension of the Flaps on the Ground Make the Thrust Reverser Unserviceable for MaintenanceFig. 401
3. Job Set-up__________
Subtask 54-55-41-941-050
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).
R Subtask 54-55-41-860-051
R B. Aircraft Maintenance Configuration
R (1) Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).
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