B.
Brake Temperature Monitor Unit (Fig. 1)
______________________________
(1)
The monitor unit is located in the E6 Aft Equipment Center. It has two plug-in printed circuit boards mounted internally which contain the system electronic circuitry. Nine light emitting diodes (LED), and a spring return test switch are mounted on the front panel of the monitor to provide test indication of the monitor unit and sensor circuit integrity.
(2)
The monitor unit senses brake temperature signals from the sensors, and produces outputs which activate various temperature indicators on the airplane.
(a)
Continuous brake temperature signals are provided to the EICAS system for display on the flight compartment P2 panel. 1) Temperature values range from 0 to 9 on the display
corresponding to a brake temperature range of 100 to 650°C (212 to 1202°F).
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MAINTENANCE MANUAL
FWD
SEE A BRAKE
A
A MAIN GEAR BRAKE
BRAKE TEMPERATURE SENSOR
T591 NO. 1 BRAKE TEMP SENSOR
(TYPICAL-8 PLACES)
A-A
A
SENSOR
FASTENER
(2 PLACES)
PLACARD
BRAKE ASSEMBLY (REF) ELECTRICAL CONNECTOR
FWD
Brake Temperature System Component Location
Figure 1 (Sheet 1)
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MAINTENANCE MANUAL
INDICATOR LIGHT
SELECTOR
MONITOR BRAKE TEMPERATURE
MAINTENANCE INSTRUCTIONS R 8765 432 SENSOR TESTTEST MONITOR MONITOR GEARGEAR L SENSORS 1
AFT EQUIPMENT CENTER BRAKE TEMPERATURE
(E6 RACK) MONITOR UNIT
Brake Temperature Monitoring System Component Location
Figure 1 (Sheet 2)
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2) The indicated numbers are displayed with a surrounding box. Either or both the digits and boxes can be shown in blue or white color, dependent on the temperature condition. The color blue indicates a normal condition and white either a threshold or high temperature condition. 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(86)