32-09-00
ALL ú ú 01 Page 2 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CONDUIT
SENSOR
SEE A
CONDUIT
TARGET
SENSOR
A
Nose Gear Air Sensing Proximity Sensor Figure 2
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-09-00
ALL ú ú 01 Page 3 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
MAIN LANDING GEAR SAFETY SENSORS - REMOVAL/INSTALLATION
_______________________________________________________
1. General_______
A. This procedure has two tasks. One task is the removal of the main landing gear safety sensors (refered to as safety sensor). The other is the installation of the safety sensors.
B. The safety sensors are found on the interlock valve support of the ground spoiler.
TASK 32-09-01-004-001
2. Main Landing Gear Safety Sensors Removal (Fig. 401)________________________________________
A. Special Tools and Equipment
(1)
Ground Locks - F72735 (Ref 32-00-01/201)
B.
References
(1)
32-00-01/201, Ground Locks
C.
Access
(1)
Location Zone
310 Left Main Landing Gear
410 Right Main Landing Gear
D.
Procedure
FWD
INBD
Main Landing Gear Safety Sensors Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-09-01
ALL ú ú 01 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AIR SAFETY SENSOR SENSOR LEADS
MOUNTING
BRACKET
TELEFLEX CABLE ACTUATORS
GROUND SAFETY
SENSOR
MOUNTING
BRACKET
VALVE
LINKAGE
GROUND SPOILER INTERLOCK VALVE
NOTE: SHOWN WITH SENSOR COVER REMOVED
B
FWD
ELECTRICAL
CONNECTOR
SYSTEM
B
RESERVOIR
INBD
FWD
GROUND SPOILER FORWARD WHEEL WELL
CONTROL MODULE BULKHEAD
C
Landing Gear Safety Sensors Adjustment Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-09-01
ALL ú ú 01 Page 402 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 864-002
WARNING:_______ MAKE SURE THAT ALL PERSONS AND EQUIPMENT ARE KEPT AWAY FROM THE
CONTROL SURFACES. THE CONTROL SURFACES WILL MOVE AUTOMATICALLY
DURING MAINTENANCE IF THE HYDRAULIC SYSTEM A OR B IS
PRESURIZED. THIS CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO
EQUIPMENT.
(1)
Keep all persons and equipment away from the control surfaces. S 044-003
(2)
Open all the circuit breakers for the landing gear on the circuit breaker panel, P6-2.
S 494-004
(3)
Make sure the ground locks are installed in all the landing gear (Ref 32-00-01/201).
S 014-018
(4)
Remove the sensor cover. S 024-005
(5)
Remove the sensor from the mounting bracket. S 034-006
(6)
Remove the sensor wire clamp from the interlock valve bracket. S 034-007
(7)
Remove the sensor wires from the wire bundle. S 034-008
(8)
Disconnect the electrical connector.
(a)
Write the location of the wire color codes. NOTE: Do this to make the installation of the new sensor
____ easier.
(b)
Disconnect the electrical connector. NOTE: The electrical connector is found at the right body
____ station 675. 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 起落架 LANDING GEAR 1(13)
