S 794-083
(7)
After five minutes do a visual check of the valve installation for leaks.
S 714-106
(8)
Do a check for correct brake operation as follows:
(a)
Push in the brake pedals fully and release them while you watch the brakes operate.
(b)
Look to see that the brake pistons move (The brake pistons will extend when the brake is applied and will retract when the brake is released).
S 944-107
(9) Do the steps in the Restore Airplane to Normal paragraph if more maintenance is not necessary.
TASK 32-42-03-944-084
11. Return the Airplane to Its Usual Condition
__________________________________________
A. References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 29-11-00/201, Pressurize/Depressurize Main Hydraulic System
(3)
AMM 25-50-03/401, Bulkhead Lining
(4)
AMM 32-00-15/201, Landing Gear Door Locks
B.
Access
(1)
Location Zones
143 Left Main Landing Gear Wheel Well
144 Right Main Landing Gear Wheel Well
211/212 Control Cabin
C.
Procedure
(1)
Set the parking brake.
S 864-086
(2)
Remove the pressure from the right and left hydraulic systems if it is not necessary (AMM 29-11-00/201).
S 864-085
S 094-087
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.
(3) Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
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(4) S 414-103Install the access panel on the E5 rack that is located on the forward bulkhead of the forward cargo compartment (AMM 25-50-03/401).
(5) S 414-104Close the forward cargo door, 821.
(6) S 864-105Remove electrical power if it is not necessary (AMM 24-22-00/201).
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ANTISKID TRANSDUCER DRIVE - REMOVAL/INSTALLATION
________________________________________________
1. General_______
A. The antiskid transducer drive has a coupling assembly, mounting plate, cup and a pad washer. All the components of the antiskid transducer drive (this does not include the dog and cone washer) are installed in the hubcap of each main landing gear wheel. The dog and the cone washer (part of the transducer assembly) are installed on the transducer rotor shaft.
B. This procedure contains two tasks. The first task removes the antiskid transducer drive. The second task installs the antiskid transducer drive.
TASK 32-42-04-004-001
2. Remove the Antiskid Transducer Drive (Fig. 401)____________________________________
A. References
(1)
32-00-20/201, Landing Gear Downlocks
B.
Access
(1)
Location Zones
731 Main Landing Gear (MLG) (Left)
741 Main Landing Gear (MLG) (Right)
C.
Procedure
S 214-008
(1)
Make sure the downlocks are installed on the nose and main landing gear (Ref 32-00-15).
(2)
Make sure there are chocks on the wheels.
S 024-023
(3)
Remove the antiskid transducer drive on airplanes with metal hubcaps as follows:
(a)
Remove the three hubcap mounting bolts (8), washers (13) and nuts (14).
S 214-009
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2. PLATE 3. COUPLING ASSEMBLY 4. CUP 5. PAD WASHER (2 LOCATIONS) 6. SCREW
FWD 1. HUBCAP 7. BOLT (4 LOCATIONS)
A ANTISKID TRANSDUCER DRIVE SEE (2 LOCATIONS) 9. BOLT
MOUNTING 8. HUBCAP BOLT (3 LOCATIONS)
ASSEMBLY (REF) TRANSDUCER
(REF) (REF) CONE WASHER DOG WHEEL (REF)
14. NUT
13. WASHER
A ANTISKID TRANSDUCER DRIVE
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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 3(35)
