(e)
Pull the sensor and mounting adapters out of the axle.
(f)
Put marks on the outboard and inboard mounting adapters to show location in the axle.
NOTE: You may reuse only properly identified mounting
____
adapters.
S 034-013
(5) Remove the mounting adapters from the sensor (Fig. 403):
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A
747-400
MAINTENANCE MANUAL
SEE A
13. INBOARD
MOUNTING 1. NAMEPLATE
ADAPTER ATTACHMENT
12. INBOARD RING
SEE B
11. OUTBOARD
10. INBOARD RING
MOUNTING BOLT (CAPTIVE) FWD
1
9. NULL ADJUSTMENT OUTBOARD
CAM MOUNTING BOLT
8. OUTBOARD NULL ADJUSTMENTMOUNTING CAM
ADAPTER 1
2. CABLE GUIDE TUBES
3. CABLE GUIDE ASSEMBLY
4. ELECTRICAL CONNECTOR
5. ELECTRICAL CABLE
6. OUTBOARD ANTIROTATION
WASHER MOUNTING BOLT 7. OUTBOARD
INSTALL SENSOR WITH MASTER KEY AS SHOWN IN-AXLE MOUNT RINGS WITH LOAD SENSORS INSTALLED
1
Nose Landing Gear Load Sensor Installation Figure 402 (Sheet 1)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
INBOARD MOUNTING
IN-AXLE MOUNT RINGS
Nose Landing Gear Load Sensor Installation
Figure 402 (Sheet 2)
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C79507
A
747-400 MAINTENANCE MANUAL
CAUTION: DO NOT HOLD THE ADAPTER SPRING TANGS (3) WITH THE VISE.
_______ THE VISE CAN CAUSE DAMAGE TO THE SPRING TANGS.
(a)
Put the inboard mounting adapter (5) in a vise and support free end to prevent stretching the sensor bellows.
(b)
Remove the sensor mounting bolt and washer (1) from the inboard mounting adapter (5).
(c)
Remove the sensor from the inboard mounting adapter (5).
(d)
Remove the inboard mounting adapter (5) from the vise.
(e)
Put the outboard mounting adapter (4) in the vise.
(f)
Remove the sensor mounting bolt and washer (1) from the outboard mounting adapter (4).
(g)
Remove the sensor from the outboard mounting adapter (4).
(h)
Remove the outboard mounting adapter (4) from the vise.
(i)
Keep the used mounting adapters (4,5) and the used sensor mounting bolts and washers (1). You will use these items again.
TASK 31-41-06-404-015
3. Nose Landing Gear Load Sensor Installation
__________________________________________
A. General
(1) After the installation of a load sensor you must adjust the sensor zero. There are two zero adjustment procedures. It is necessary to do only one of the two adjustment procedures. One procedure does not require the airplane to be on jacks. The other procedure requires the airplane to be on jacks. Both procedures use the keyboard modes of the weight and balance computer (WBC).
(a)
After sensor installation, do the automatic zero adjustment (without jacks, mode 38) if you replaced only one sensor on the nose landing gear.
(b)
After sensor installation, do the zero adjustment on jacks (mode 99) if you replaced two or more sensors on the nose landing gear.
B. References
(1) AMM 07-11-03/201, Jacking Airplane Axles
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本文链接地址：747-400 AMM 飞机维护手册 指示/记录系统 1(128)
