A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵2(17)

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R  (0.5590 in.). 
R  NOTE : If the axial play is less than the given limit, the bolts (3)____ 
R  can be less than the minimum dimension of 14.20 mm (0.5590 
R  in.). 
R  (4) Measure the axial play between the bushes (1) and their related bolt 
R  (3) at the rudder fitting. 
R  (5) Make sure that the axial play is a maximum of 0.158 mm (0.0062 in.). 
R  (6) Make sure that the bolt (3) has a minimum diameter of 14.20 mm 
R  (0.5590 in.). 
R  NOTE : If the axial play is less than the given limit, the bolt (3)____ 
R  can have a minimum diameter of less than 14.20 mm (0.5590 
R  in.).
 5. Close-up________
 Subtask 27-21-41-410-052
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other
 items.
 (2) Install the rudder (Ref. TASK 27-21-41-400-001).

 

 Subtask 27-21-41-942-055
 B. Put the aircraft back to the serviceable condition.
 (1)
 Remove the warning notice(s).

 (2)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 

 PEDALS - REMOVAL/INSTALLATION
_____________________________ TASK 27-21-42-000-001 Removal of the CAPT Pedals 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 notices
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-21-43-000-002 Removal of the Pedal Position Adjuster Assembly 27-21-42-991-001 Fig. 401 27-21-42-991-002 Fig. 402

 3. Job Set-up
__________ Subtask 27-21-42-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Remove the pedal position adjuster assembly (Ref. TASK 27-21-43-000-002).

 (2)
 Put the warning notices on the pedals (CAPT and F/O) to tell persons not to operate them.

 4. Procedure
_________ (Ref. Fig. 401/TASK 27-21-42-991-001, 402/TASK 27-21-42-991-002) Subtask 27-21-42-020-052
 A. Removal of the Pedal Assembly
 (1)
 Remove the cotter pin (2) and discard it. Remove the nut (5), the bonding strip (4), the washer (3) and the bolt (1) (ref. Detail B).

 (2)
 Remove the cotter pin (25) and discard it. Remove the nut (26), the washer (27) and the bolt (40). Disengage the rod (28) from the bellcrank (41) (Ref. Detail E).

 NOTE : Apply a force on the left or right pedal (29) to simulate a
____ brake application. This gives a free passage to the bolts (39) and (40) (Movement of the bellcranks (35) and (41)).
 (3)
 Remove the cotter pin (38) and discard it. Remove the nut (37), the washer (36) and the bolt (39). Disengage the rod (34) from the bellcrank (35) (Ref. Detail E).

 (4)
 Remove the cotter pin (16) and discard it. Remove the nut (15), the washer (14) and the bolt (17). Disengage the rod (12) from the bellcrank (13) (Ref. Detail D).

 (5)
 Remove the cotter pin (6) and discard it. Remove the nut (7), the washer (8) and the bolt (11). Disengage the rod (9) from the bellcrank (10) (Ref. Detail C).

 (6)
 Remove the nuts (33) and discard them. Remove the bolts (31) (Ref. Detail F).

 (7)
 Remove the bushes (30) and remove the pedal assembly (29) from the

 

 

 CAPT Pedals
 Figure 401/TASK 27-21-42-991-001
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 CAPT Pedals
 Figure 402/TASK 27-21-42-991-002
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