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LANDING GEAR POSITION INDICATING AND WARNING SYSTEM - ADJUSTMENT/TEST
_____________________________________________________________________
1. General
A. This task does a test of the position indication and warning system for the landing gear. It is necessary to lift the airplane on jacks to let the landing gear retract and extend.
TASK 32-61-00-725-001
2. Test of the Landing Gear Position Indicating and Warning System
_______________________________________________________________
A. Special Tools and Equipment
(1)
Airplane Jacks (Ref 07-11-11/201)
(2)
Ground Locks - F72735 (Ref 32-00-01/201)
(3)
Hydraulic test bench capable of delivering 20 gpm at 3000 psi
NOTE: You can also use airplane hydraulic power, but you cannot
____
control the hydraulic pressure.
B. References
(1)
07-11-11/201, Jack Airplane
(2)
24-22-00/201, Manual Control
(3)
29-15-00/201, Hydraulic Systems A, B, and Standby
(4)
32-00-01/201, Ground Locks
C.
Access
(1)
Location Zones
101 Control Cabin
102 Control Cabin
204 Nose Gear
310 Left Main Landing Gear
410 Right Main Landing Gear
D.
Prepare to Do the Test
S 495-002
(1)
Make sure the ground locks are installed in all the landing gear (Ref 32-00-01/201).
S 585-003
(2)
Lift the airplane on jacks until all the tires are clear of the ground (Ref 07-11-11/201).
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本文链接地址：737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 3(151)
