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WHEEL WELL FORWARD WALL
D
C D
C
FWDFORWARD DOOR OPERATING MECHANISM (REF)
NOSE GEAR DOOR CLOSED SENSORS NOSE GEAR DOOR
CLOSED SENSORS
SEE D
D
SENSOR
BRACKET
(REF) NOSE GEAR DOOR CLOSED SENSOR S10243, SYS 1
WHEEL WELL FORWARD WALL (REF)
DOOR SEAL (REF)
NOSE GEAR
TARGET (REF)
DOOR (REF) C-C
SENSOR
BRACKET NOSE GEAR DOOR
(REF) CLOSED SENSOR
FORWARD WHEEL WELL S10081, SYS 2
WALL (REF)
DOOR SEAL (REF) NOSE GEARTARGET (REF)
D-D
DOOR (REF)
Component Location Figure 102 (Sheet 3)
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FLEXIBLE
LOCK LINK CONDUIT
ASSY (REF) (REF)
SEE E
MAIN LANDING GEAR
DOWN AND LOCKED
SENSOR
LH S10061, SYS 1
LH S10074, SYS 2
RH S10057, SYS 1
LEFT MAIN GEAR RH S10070, SYS 2
(RIGHT SIMILAR)
UPPER LOCK LINK (REF) TARGET SENSOR LOWER LOCK LINK (REF)
(REF)
MLG DOWN AND LOCKED SENSORS
F
CONNECTOR
BRACKET (REF)
LOCK
ACTUATOR
(REF)
LOCK LINK
ASSEMBLY
(REF)
REAR SPAR
(REF) CONNECTOR
DISCONNECT
FLEXIBLE CONDUIT (REF) FWD
(REF)
MLG DOWN AND INBD
LOCKED SENSORS
SEE F LOCK LINK ASSY (REF)
E
Component Location
Figure 102 (Sheet 4)
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L OR R MAIN GEAR UPLOCK ASSEMBLY
SEE G
MLG UP AND
LOCKED SENSORS
SEE G
FWD
LEFT MAIN STRUCTURE
WHEEL WELL OUTBOARD WALL
(REF)
(RIGHT SIMILAR)
MLG UP AND LOCKED SENSOR S10240, SYS 1, LH S10239, SYS 1, RH
MLG UP AND UP LOCK
LOCKED SENSOR ASSEMBLY
S10073, SYS 2, LH (REF)S10069, SYS 2, RH
LEFT SHOWN, RIGHT OPPOSITE
G MLG UP AND
G-G
LOCKED SENSOR
G
MAIN GEARUPLOCK HOOK (REF)INBD
L MAIN GEAR UPLOCK ASSEMBLY (RIGHT SIMILAR)
G
Component Location
Figure 102 (Sheet 5)
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SEE MLG DOOR CLOSED SENSORS H WALL (REF) MAIN WHEEL WELL OUTBOARD
SENSOR BRACKET (REF)
G G
DOOR STOP (REF) F F
FWD OUTER BODY SKIN (REF) MLG DOOR CLOSED SENSORS (LEFT SHOWN, RIGHT OPPOSITE)
H
TARGET (REF) SENSOR BRACKET (REF) CLOSED SENSOR MLG DOOR L, S10242, SYS 1 R, S10241, SYS 1 SENSOR BRACKET (REF)
MLG DOOR
CLOSED SENSOR MAIN LANDING MAIN LANDING DOOR SEAL
L, S10076, SYS 2 GEAR DOOR GEAR DOOR (REF) (REF)
R, S10072, SYS 2 OUTER SKIN (REF)
F-F G-G
Component Location
Figure 102 (Sheet 6)
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LANDING GEAR POSITION INDICATING AND WARNING SYSTEM - ADJUSTMENT/TEST
_____________________________________________________________________
1. General_______
A. The procedure has two tasks:
(1)
System Test of the Landing Gear Position Indication System
(2)
Inductance and Resistance Test of the Proximity Sensors
(a)
This task electrically tests the sensors. This test measures sensor resistance and inductance to identify a bad sensor.
B.
Adjustment of the position indication proximity sensors is given in the procedures that follow:
(1)
Main Gear Proximity Sensors (AMM 32-61-02/201).
(2)
Nose Gear Proximity Sensors (AMM 32-61-03/201).
TASK 32-61-00-705-001
2. System Test - Landing Gear Position Indication System (Fig. 501)_____________________________________________________
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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(145)
