(7)
Lower the door and remove it.
TASK 32-12-01-404-012
3. Install the Door for the Main Landing Gear (Fig. 401)
__________________________________________
A. Equipment
(1) Handling Equipment, MLG Door and AC Door -
B32043-1 ú (2) Lift Fixture, Engine Accessory - A71015-87
B. Parts
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MAINTENANCE MANUAL
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT |FIG | ITEM | ................................................................................ | 401 | 1 | Pin | 32-32-12 | 01 | 10 | | | 5 | Nut | | | 25 | | | 7 | Bolt | 32-12-01 | 01 | 10 | | | 9 | Washer | | | 15 | | | 13 | Nut | | | 35 | | | 15 | Washer | | | 30 | | | 16 | Hinge Pin | | | 25 | 2......…........…...................................…...........…....….........1
C. References
(1)
AMM 32-00-15/201, Landing Gear Door Locks
(2)
AMM 32-12-00/501, Main Gear Doors
D.
Access
(1)
Location Zones
731/741 Main Landing Gear (MLG)
732/742 MLG Body Doors
733/743 MLG Oleo Doors
E.
Install the door
S 864-024
(1)
Lower the handling equipment.
S 864-025
(2)
Lift the fixture to move the door into position for the installation.
S 414-014
(3)
Install the hinge pin (16), the washers (15), the nuts (13), and the cotter pins to connect the door (12) to the forward and aft hinge
(8)
(View C-C).
(a)
Tighten the nuts. Do not apply a torque to the nut. Loosen it a maximum of 1/6 of a turn to install the cotter pin.
S 414-015
(4)
Install the hinge bolts (7), the washers (9), the nuts (10), and the cotter pins to connect the door (12) to the forward and aft hinge
(8)
(View B-B).
(a)
Tighten the nuts. Do not apply a torque to the nut. Loosen it a maximum of 1/6 of a turn to install the cotter pin.
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F. Put the Airplane Back to Its Usual Condition
S 094-016
(1)
Remove the handling equipment and the lift fixture.
S 434-017
(2)
Attach the bonding jumpers (11) to the door hinges (8).
S 434-018
(3)
Install the pin (1) to connect the rod end of the door actuator (3) to the door beam (6).
(a)
Do not permit the pin (1) to come out of the hole.
(b)
Do not install the nut (5) until the actuator adjustment is completed.
S 824-026
(4) Adjust the door for the main landing gear and adjust the door actuator (AMM 32-12-00/501).
S 094-027
WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(5) Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
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MAIN GEAR DOOR TANG - REMOVAL/INSTALLATION
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本文鏈接地址：757 AMM 飛機維護手冊 起落架 CHAPTER 32 - LANDING GEAR 1(154)
