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时间:2011-03-27 00:00来源:蓝天飞行翻译 作者:admin
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R **ON A/C 001-003, 051-054,
 52-33-12-991-001 Fig. 401 R **ON A/C 004-049, 055-099, 101-149, 221-221, 224-224, 228-228,
 52-33-12-991-001-A Fig. 401A
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R  **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 3. Job Set-up__________ Subtask 52-33-12-010-050
 A. Get Access
 (1) Put the access platform in position below the Bulk cargo-compartment door (referred to as Bulk door). (2) Open the AFT cargo-compartment door (Ref. TASK 52-30-00-860-001). (3) Remove the divider net between the AFT/Bulk cargo compartment at FR59.
 (4) Remove the door net from the opening of the Bulk cargo compartment. (5) Remove the insulation packs from the fuselage around the forward and aft hinge frames. 4. Procedure_________
 Subtask 52-33-12-020-050
R  A. Removal of the FWD and the AFT Support Arms **ON A/C 001-003, 051-054,
R  (Ref. Fig. 401/TASK 52-33-12-991-001) **ON A/C 004-049, 055-099, 101-149, 221-221, 224-224, 228-228,
R  (Ref. Fig. 401A/TASK 52-33-12-991-001-A) **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 NOTE : The procedure for the AFT and the FWD support arm is the same.____ (1) Remove the BULK door (Ref. TASK 52-33-11-000-001). (2) Remove the nut (12) and the washer (11) from the bolt assembly (8) mounted on the door structure. 

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 Suspension Arm
 Figure 401/TASK 52-33-12-991-001

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 Suspension Arm
 Figure 401A/TASK 52-33-12-991-001-A

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 (3)
 Remove the nut (4), the bolt (1), and the bonding jumpers (5) and (2) from the bracket (13).

 (4)
 Remove the hinge pin (6) from the support arm (3) as follows:

 (a)
 Remove the screw (20) and the tab washer (21) from the bracket (22).

 (b)
 Remove and discard the tab washer (21) from the screw (20).

 (c)
 Remove the hinge pin (6) from the support arm (3).

 

 (5)
 Remove the support arm (3) from the bracket (22) and the bolt assembly (8).

 (6)
 Remove the plug (10) from the support arm (3).

 (7)
 If necessary, remove the nuts (7), the bolts (9) and the bolt assembly (8) from the door structure.


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 TASK 52-33-12-400-001 Installation of the Door Suspension
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  access platform 2.3 m (7 ft. 7 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-027  USA MIL-L-81309
 RUST INHIBITOR(FOR CORROSION USE 15-004)
 (Ref. 20-31-00)
 Material No. 09-018  USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
10 plug 52-33-12 01 -060 21 tab washer 52-33-12 01 -120
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 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
 Yellow Electric Pump 52-30-00-860-008 Close the Bulk Cargo-Compartment Door 52-30-00-860-011 Close the Deactivated Bulk Cargo-Compartment Door 52-33-11-400-001 Installation of the Bulk Cargo-Compartment Door
 
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