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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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R R  (2) Remove the bonding jumpers (8) from the upper fuselage at FR53 and FR55A as follows: 
R  (a) Remove the screws (6), the washers (7) from the upper door frame. 
R  (b) Remove the bonding jumpers (8) from the upper door frame. 
R  (3) Disconnect the door actuators from the cargo door as follows: 
R R  (a) Remove the nut (9), the washer (11), the bolt (12) and the bonding jumper (10) from the actuator attachment fitting (13). 
R R  (b) Remove the cotter pin (17), the nut (16) and the washer (15) from the bolt (14). 
R R  (c) Hold the piston eye end (18) so that it cannot fall when you remove the bolt (14). 
R R  (d) Remove the bolt (14) with the washer (15) and disconnect the piston eye end (18) from the actuator attachment fitting (13). 

R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-32-11Page 410 1301-399, 1May 01/05 1 1 1CES 1


 (4)
 Remove the screws (22) and the end fittings (23) with the shims (29) from the piano hinge area.

 (5)
 Apply masking material to the adjacent fuselage area to prevent damage during the removal of the hinge pins (24).

 (6)
 Make sure that the sling (5) is tight and that there is no load on the hinge pins (24).

 (7)
 Remove the SUPPORT STRUT - CARGO DOORS (98D52307524000) from the cargo door.

 (8)
 Remove the hinge pins (24) and the washers (25 thru 28) from the piano hinge area with EXTRACTOR - HINGE PINS, CARGO DOOR (98D52307523000).

 (9)
 Carefully remove the cargo door from the fuselage and put it in an applicable fixture.


R **ON A/C 151-199, 401-499,
 Subtask 52-32-11-020-050-A
 A. Removal of the Cargo door
 (1)
 Remove the wire harness 4613VB from the fuselage as follows:

 (a)
 Disconnect the electrical connector (20) from the receptacle (19).

 (b)
 Put blanking caps on the electrical connector (20) and the receptacle (19).

 (c)
 Loosen the cable clamps and remove the cable loom (21) from the ceiling lining in the door actuator area.

 

 (2)
 Disconnect the door actuators from the cargo door as follows:

 (a)
 Remove the nut (9), the washer (11), the bolt (12) and the bonding jumper (10) from the actuator attachment fitting (13).

 (b)
 Remove the cotter pin (17), the nut (16) and the washer (15) from the bolt (14).

 (c)
 Hold the piston eye end (18) so that it cannot fall when you remove the bolt (14).

 


R 1EFF : 051-052, 151-199, 401-499, 1 52-32-11Page 411 1 1 Aug 01/05 1 1 1CES 1


 (d)
 Remove the bolt (14) with the washer (15) and disconnect the piston eye end (18) from the actuator attachment fitting (13).

 (e)
 If neccesary, remove the bushes (22) and (23) from the actuator attachment fitting (13).


 (3)
 Remove the screws (22) and the end fittings (23) from the piano hinge area.

 (4)
 Apply masking material to the adjacent fuselage area to prevent damage during the removal of the hinge pins (24).

 (5)
 Make sure that the sling (5) is tight and that there is no load on the hinge pins (24).

 (6)
 Remove the SUPPORT STRUT - CARGO DOORS (98D52307524000) from the cargo door.

 (7)
 Remove the hinge pins (24) and the washers (25 thru 28) from the piano hinge area with EXTRACTOR - HINGE PINS, CARGO DOOR (98D52307523000).

 (8)
 Carefully remove the cargo door from the fuselage and put it in an applicable fixture.


 **ON A/C ALL
 5. Close-up
________ Subtask 52-32-11-942-050
 A. Preparation of the Cargo Door for the Stowage
 (1)
 Remove the sling (5) from the cargo door.

 (2)
 Remove the hoisting lugs (2) from the cargo door and install them again with the eye-end inboard.


 1EFF : ALL 1 52-32-11Page 412 1 1 May 01/05R 1 1 1CES 1


 TASK 52-32-11-400-001
 Installation of the AFT cargo Compartment Door
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific crane with a minimum capacity 130.0 kg (286.6 lb)
 No specific access platform 3.5 m (11 ft. 6 in.)
 
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