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时间:2011-03-26 23:57来源:蓝天飞行翻译 作者:admin
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 (3) Connect the link rod (1) to the deflection lever (10) as follows:
 (a)
 Put the fork end of the link rod (1) on the eye end of the deflection lever (10.

 (b)
 Install the bolt (2), the bush (3), the washer (4) and the nut


 (5) on the link rod (1).
 (c) Tighten the nut (5) and safety it with the new cotter pin (6). Subtask 52-32-21-820-054
 D. Adjustment Procedure
 (1)
 Make sure that the upper dead center of the locking mechanism is correctly adjusted (Ref. TASK 52-32-11-820-002).

 (2)
 Make sure that the proximity switch 5MJ is correctly adjusted (Ref. TASK 52-35-13-400-002).


 Subtask 52-32-21-720-053
 E. Test Procedure
 (1)
 Do a functional test of the upper dead center to make sure that the locking mechanism operates satisfactorily (Ref. TASK 52-32-00-720-001).

 (2)
 Do the functional test to make sure that the proximity switch 12MJ is correctly adjusted (Ref. TASK 52-32-00-720-001).


 5. Close-up
________ Subtask 52-32-21-865-064
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 1MJ, 3801GX, 3802GX, 3803GX.

 1EFF : 051-052, 1 52-32-21Page 487 1 1 Aug 01/05R 1 1 1CES 1


 Subtask 52-32-21-410-055
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Apply STORAGE PRESERVATION (Material No. 15-005) to all the components of the locking shaft assembly and to the adjacent cargo door structure.

 (3)
 Install the plastic plugs (36) in the lateral cutouts of the cargo door.

 (4)
 Install the access panel 826AR on the cargo door.

 (5)
 Remove the actuator safety locks and close the cargo door (Ref. TASK 52-30-00-860-002).


R 1EFF : 051-052, 1 52-32-21Page 488 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 

 TASK 52-32-21-000-006
 Removal of the Interlock Mechanism

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific access platform 3.5 m (11 ft. 6 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
52-30-00-860-001  Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 52-32-21-991-008 Fig. 408
 **ON A/C 051-052,

 52-32-21-991-008-A  Fig. 408A
R 1EFF : ALL 1 52-32-21Page 489 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL


 3. Job Set-up
__________
 Subtask 52-32-21-010-056

 A. Get Access
 (1)
 Open the AFT cargo-compartment door (referred to as cargo door) and safety it with the actuator safety locks (Ref. TASK 52-30-00-860-001).

 (2)
 Put the access platform in position below the opened cargo door.


 (3) Remove the access panel 826AR from the cargo door.
 Subtask 52-32-21-865-065

 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-32-21-860-056
 C. Aircraft Maintenance Configuration
 (1) Move the latching mechanism of the opened cargo door in the locked condition as follows:
 (a)
 Press the roller lever (263) of the interlock mechanism outboard to release the blockage of the latching shaft.

 (b)
 Move the door handle down to the locked position and push it into the recess of the door structure.


R 1EFF : ALL 1 52-32-21Page 490 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 051-052,


 Subtask 52-32-21-860-056-A
 C. Aircraft Maintenance Configuration
 
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