R (6) Install the SUPPORT STRUT - CARGO DOORS (98D52307524000) to safety
R the opened cargo door.
R (7) Remove the sling (5) from the cargo door.
R (8) Attach the end-fittings (30) and the shims (29) with the screws (31)
R to the fuselage structure.
R (9) Connect the door actuators (19) to the actuator attachment fittings
R (13) of the cargo door as follows:
R (a) If removed, install the bushes (22) and (23) into the actuator
R attachment fitting (13).
R (b) Put the piston eye end (18) to the actuator attachment fitting
R (13) and install the bolt (14) with the washer (15).
R NOTE : If you can not install the bolt (14) adjust the length of____
R the door actuator (Ref. TASK 52-31-11-820-004).
R (c) Install the washer (15) and the nut (16) to the bolt (14).
R (d) TORQUE the nut (14) to between 1.0 and 1.35 m.daN (88.49 and
R 119.46 lbf.in) and loosen it to the next cotter pin hole.
R (e) Safety the nut (14) with the cotter pin (17).
R (f) Install the bonding jumpers (10) with the bolts (12), the washers
R (11) and the nuts (9) to the actuator attachment fitting (13)
R (Ref. TASK 20-28-00-912-004).
R (10) Install the wire harness 4611VB (21) to the ceiling lining of the
R actuator area and connect the connector (20) to the receptacle (19)
R (Ref. TASK 52-31-24-400-001).
R (11) If you install bonding jumpers (8) at the cargo door, install them
R with the bolts (6) and the washers (7) to the upper fuselage at FR25
R and FR27A (Ref. TASK 20-28-00-912-004).
R NOTE : Do the Preparation for Installation Procedure.(Ref. Para. A.).____
Subtask 52-31-11-865-051
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MJ, 3801GX, 3802GX, 3803GX
Subtask 52-31-11-860-057
D. Preparation for the Test
(1)
Pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002).
(2)
Remove the SUPPORT STRUT - CARGO DOORS (98D52307524000) from the cargo door.
Subtask 52-31-11-710-050
E. Operational Test of the Cargo Door.
(1)
Close the cargo door (Ref. TASK 52-30-00-860-002). NOTE : Make sure that the cargo door closes smoothly and easily.
____
(2)
Make sure that the skin offset between the loftline of the cargo door and the fuselage contour is correct (Ref. TASK 52-31-11-820-001).
(3)
Make sure that the cargo door seal is compressed around its length.
(4)
Open the cargo door (Ref. TASK 52-30-00-860-001). NOTE : Make sure that the cargo door opens smoothly and easily.
____
5. Close-up
________
Subtask 52-31-11-910-052
A. Put the aircraft back to the serviceable condition.
(1)
Remove the hoisting lugs (2) from the cargo door and install the plastic caps again.
(2)
Apply a bead of SEALANTS (Material No. 09-016) around the end fittings (23).
1EFF : ALL 1 52-31-11Page 422 1 1 May 01/05 1 1 1CES 1
(3) Apply SPECIAL MATERIALS (Material No. 05-027) to all components which
have no other surface protection. Subtask 52-31-11-410-050
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the cargo door (Ref. TASK 52-30-00-860-002).
(3)
Remove the access platform(s).
1EFF : ALL 1 52-31-11Page 423 1 1 May 01/05 1 1 1CES 1 DOOR - CARGO COMPARTMENT - ADJUSTMENT/TEST
__________________________________________
TASK 52-31-11-820-001
Adjustment of the FWD Cargo-Compartment Door
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門4(48)
