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757
MAINTENANCE MANUAL

SEE
INDICATOR LIGHT
SELECTOR
BRAKE TEMPERATURE MONITOR UNIT
SEE

BRAKE TEMPERATURE MONITOR UNIT
E6-4

AFT EQUIPMENT CENTER (E6 RACK)

Brake Temperature Monitor Unit Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH BRAKE TEMPERATURE MONITOR ú

 32-46-01
 SYSTEM  ú
 ú  09  Page 402
 ú  May 28/99 
 

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MAINTENANCE MANUAL

 B. Access
 (1)  
Location Zones
 211 Control Cabin, Left
 212 Control Cabin, Right
 822 Aft Cargo Door

 C.
Procedure

 S 424-023
 (1)  
Install the brake temperature monitor unit in the E6 rack
 (AMM 20-10-01/401).

 S 864-026

 (2)  
Remove the DO-NOT-CLOSE tags and close this circuit breaker on the P11 panel:

 (a)  
11S26, BRAKE TEMP

 S 864-027
 (3)  
Supply electrical power (AMM 24-22-00/201).

 S 714-028

 (4)  
Do a test of the brake temperature monitor unit (AMM 32-46-00/501).

 (5)  
Close the aft cargo door, 822.

 (6)
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 S 414-029
 S 864-042
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH BRAKE TEMPERATURE MONITOR ú

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 SYSTEM  ú
 ú 08 ú   Page 403Jan 28/02 

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757 MAINTENANCE MANUAL
 BRAKE TEMPERATURE SENSOR - REMOVAL/INSTALLATION
_______________________________________________
 1.  General_______
 A.  This procedure contains two tasks. The first task removes the brake temperature sensor. The second task installs the brake temperature sensor.
 TASK 32-46-03-004-014
 2.  Remove the Brake Temperature Sensor (Fig. 401)___________________________________
 A.  References
 (1)  
AMM 32-00-20/201, Landing Gear Downlocks

 (2)  
AMM 32-41-10/401, Main Gear Wheel Brake

 B.  
Access

 (1)  
Location Zones
 211 Control Cabin, Left
 212 Control Cabin, Right
 731 Landing Gear Left
 741 Landing Gear Right

 C.  
Procedure

 S 494-007
 (1)  
Make sure that the landing gear downlocks are installed (AMM 32-00-20/201).

 S 864-008

 (2)  
Open this circuit breaker on the overhead circuit breaker panel P11 and attach a DO-NOT-CLOSE tag:

 (a)  
11S16, BRAKE TEMP

 S 034-009
 (3)  
Disconnect the electrical connector from the temperature sensor (Detail A).

 S 034-010

 (4)  
Remove the pin that attaches the brake rod to the brake assembly (AMM 32-41-10/401).

 S 014-011

 (5)  
Rotate the brake assembly approximately 45 degrees in the direction away from the brake rod to get access to the sensor attachment screws.

 (6)
Remove the two screws and remove the sensor from the brake.

 S 024-012
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH BRAKE TEMPERATURE ú

 32-46-03
 MONITORING SYSTEM  ú ú 03 Page 401 ú May 28/99
 
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757
MAINTENANCE MANUAL

SEEA
FWD
BRAKE
SENSOR MOUNTING FLAT
BRAKE ASSEMBLY
PIN BOLT
(PIN HEAD ON  BRAKE (2 LOCATIONS)
THE TRUCK SIDE) TEMPERATURE
SENSOR
BRAKE ROD

ELECTRICAL CONNECTOR
FWD
A

Brake Temperature Sensor Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH BRAKE TEMPERATURE ú
　
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