曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

ONE WHEEL AND TIRE ASSEMBLY FROM THE
NOSE LANDING GEAR AT A TIME. IF YOU
REMOVE THE TWO WHEEL AND TIRE
ASSEMBLIES AT THE SAME TIME, STRUCTURAL
DAMAGE AND INJURY TO PERSONS CAN OCCUR
IF THE AIRPLANE FALLS.
TIRES AND WHEELS - NOSE LANDING GEAR WHEEL AND TIRE
EFFECTIVITY
GUN ALL 32-45-00
Page 8
D633A101-GUN Oct 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-45-00-003
TIRES AND WHEELS - NOSE LANDING GEAR WHEEL AND TIRE
TIRES AND WHEELS - NOSE LANDING GEAR WHEEL AND TIRE
EFFECTIVITY
GUN ALL 32-45-00
Page 9
D633A101-GUN Feb 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-45-00-003
Purpose
Two nose wheel spin brakes use friction with the nose tires to
stop nose wheel rotation after the nose landing gear retracts
into the wheel well.
Physical Description
The nose wheel spin brake assemblies attach to spring
supports in the upper forward nose landing gear wheel well.
You can replace the wear pads on each assembly. The wear
pads do not have asbestos in the pads.
TIRES AND WHEELS - NOSE LANDING GEAR WHEEL SPIN BRAKE
EFFECTIVITY
GUN ALL 32-45-00
Page 10
D633A101-GUN Oct 10/2002
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-45-00-004
TIRES AND WHEELS - NOSE LANDING GEAR WHEEL SPIN BRAKE
TIRES AND WHEELS - NOSE LANDING GEAR WHEEL SPIN BRAKE
EFFECTIVITY
GUN ALL 32-45-00
Page 11
D633A101-GUN Feb 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-45-00-004
THIS PAGE IS INTENTIONALLY LEFT BLANK
32-46-00
Page 1
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Purpose
The brake temperature monitoring system monitors the
temperature of each main landing gear brake.
Brake Temperature Indication
Brake temperature shows on the lower systems display unit.
An amber BRAKE TEMP light gives the indication of a high
brake temperature condition.
BRAKE TEMPERATURE MONITORING SYSTEM - INTRODUCTION
EFFECTIVITY
GUN 201-999 32-46-00
Page 2
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-46-00-001
BRAKE TEMPERATURE MONITORING SYSTEM - INTRODUCTION
BRAKE TEMPERATURE MONITORING SYSTEM - INTRODUCTION
EFFECTIVITY
GUN 201-999 32-46-00
Page 3
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-46-00-001
Purpose
The brake temperature monitoring system monitors the
temperature of each main landing gear brake, provides a
temperature indication of each main gear brake, and warns of
brake high temperature conditions.
Components
These are the brake temperature monitoring system
components:
* Temperature sensor (4)
* Brake temperature monitoring unit
* Brake temperature display
* BRAKE TEMP light.
BRAKE TEMPERATURE MONITORING SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
GUN 201-999 32-46-00
Page 4
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-46-00-002
BRAKE TEMPERATURE MONITORING SYSTEM - GENERAL DESCRIPTION
BRAKE TEMPERATURE MONITORING SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
GUN 201-999 32-46-00
Page 5
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-46-00-002
Purpose
The brake temperature sensors supply brake temperature data
to the brake temperature monitoring unit (BTMU).
Location
There are four brake temperature sensors. Each main landing
gear brake has a sensor in the brake housing.
Physical Description
The brake temperature sensors are at the 5:00 position in each
brake with two bolts. The sensor assembly consists of the bimetal
thermocouple, mounting flange, and connector.
The brake temperature sensors are capable of brake
temperature measurement from 100F to 1200F.
The sensors are interchangeable between brakes. The sensors
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NGAMM7(51)