* SEE WM EQUIPMENT LIST
Component Index
Figure 101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. GUN 051 ú
32-46-00
ú ú 07 Page 101 ú Dec 20/93
A
757 FAULT ISOLATION/MAINT MANUAL
BRAKE TEMP INDICATOR, L530
SEE A
P11 PANEL P3 PANEL
BRAKE TEMPERATURE
SENSORS
SEE B
FLT COMPT
BRAKE TEMPERATURE SENSOR
BRAKE NO. 1, TS91
BRAKE NO. 2, TS92
BRAKE NO. 3, TS95
BRAKE NO. 4, TS96
BRAKE NO. 5, TS93
BRAKE BRAKE NO. 7, TS97 BRAKE NO. 6, TS94
TEMP BRAKE NO. 8, TS98
W OTHERS SIMILAR) (BRAKE NO. 1 SENSOR SHOWN,
BRAKE TEMP INDICATOR, L530
A
BRAKE (REF)
TS91 NO. 1 BRAKE
TEMP SENSOR
BRAKE TEMPERATURE SENSOR(S) B
Component Location Figure 102 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. GUN 051 ú
32-46-00
ú ú 04 Page 102 ú Dec 20/93
A
757 FAULT ISOLATION/MAINT MANUAL
BRAKE TEMPERATURE MONITOR UNIT, M115
D
Component Location Figure 102 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. GUN 051 ú
32-46-00
ú ú 09 Page 103 ú Dec 20/93
A
757 MAINTENANCE MANUAL
BRAKE TEMPERATURE MONITORING SYSTEM - ADJUSTMENT/TEST
_____________________________________________________
1. General_______
A. This procedure contains two tasks. The first task is a BITE test of the brake temperature monitoring system. The second task is a a test to make sure that each brake temperature sensor is connected to the correct wheel.
B. The BITE test is a self test of the brake temperature monitoring system. the BITE test has a monitor test and a sensor test.
(1)
The monitor test is a test of operation of the monitor unit and the electrical circuits that show the brake temperature indications.
(2)
The sensor test is a test of the electrical circuit between the monitor unit and the sensors, and the electrical circuit of the sensors.
C.
This procedure also has a test to make sure that each brake temperature sensor operates. The test is only necessary when the main gear or the truck assembly for the main gear has been replaced.
TASK 32-46-00-715-001
2. Do the Brake Temperature Monitoring System Test (Fig. 501)_______________________________________________
A. References
(1)
AMM 06-46-00/201, Entry, Service, and Cargo Doors
(2)
AMM 24-22-00/201, Electrical Power - Control
(3)
AMM 31-41-00/501, Engine Indicating and Crew Alerting System (EICAS)
B.
Prepare to Do the Test
(1)
Supply electrical power (AMM 24-22-00/201).
S 865-003 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:757 AMM 飞机维护手册 起落架 CHAPTER 32 - LANDING GEAR 3(89)