B. Aircraft Maintenance Configuration
 (1)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 5. Close-up
________ Subtask 32-47-00-942-052
 A. Removal of Equipment
 (1) Remove the warning notice(s).
 1EFF : ALL 1 32-47-00Page 503 1 1 Feb 01/98 1 1 1CES 1

 SENSOR - BRAKE TEMPERATURE (4GW,5GW,6GW,7GW) - REMOVAL/INSTALLATION
___________________________________________________________________
 TASK 32-47-15-000-001
 Removal of the Brake Temperature Sensor (4GW,5GW,6GW,7GW)
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking cap
 No specific circuit breaker(s) safety clip(s)
 No specific warning notice

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 32-47-15-991-001-A Fig. 401
 **ON A/C 301-399,
 32-47-15-991-001-C Fig. 401A
 1EFF : ALL 1 32-47-15Page 401 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 32-47-15-865-050

 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU HYDRAULIC/BRK/TEMP/DET/UNIT 1GW M37
 Subtask 32-47-15-941-052
 B. Safety Precautions
 (1) Put the warning notice in the cockpit to tell persons not to operate the landing gears.
 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 32-47-15-991-001-A)
 **ON A/C 301-399,

 (Ref. Fig. 401A/TASK 32-47-15-991-001-C) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 32-47-15-020-050
 A. Removal of the Brake Temperature Sensor
 (1)
 Disconnect the connector (3) from the temperature sensor (1).

 (2)
 Put a blanking cap on the connector (3).

 (3)
 Cut and remove the lockwire from the screw (2).

 (4)
 Remove the screw (2).

 1EFF : ALL 1 32-47-15Page 402 1 1 Aug 01/05 1 1 1CES 1

 Brake Temperature Sensor Figure 401/TASK 32-47-15-991-001-A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-47-15Page 403 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R Brake Temperature Sensor
R Figure 401A/TASK 32-47-15-991-001-C12 (SHEET 1)

 1EFF : 301-399, 1 32-47-15Page 404 1 1 Feb 01/05 1 1 1CES 1

R Brake Temperature Sensor
R Figure 401A/TASK 32-47-15-991-001-C22 (SHEET 2)

R 1EFF : 301-399, 1 32-47-15Page 405 1 1 Feb 01/05 1 1 1CES 1 1EFF : ALL 1 32-47-15Page 406 1 1 Feb 01/05 1 1 1CES 1 **ON A/C ALL

 (5) Release the temperature sensor (1) from its housing along its axis.
 (6) Put a blanking cap in the temperature sensor housing. 
R  **ON A/C 301-399, 
R  Subtask 32-47-15-020-050-A 
R  A. Removal of the Brake Temperature Sensor 
R  (1) Disconnect the connector (2) from the temperature sensor (1). 
R  (2) Put a blanking cap on the connector (2). 
R  (3) Remove the screw (3), remove and discard the washer (4). 
R  (4) Pre SIL 32-0106 
R  (a) Loosen the sensor assembly screw (5) from the retainer 
R  subassembly (6). 
R  (b) Remove the end of the BTMS sensor assembly from the pressure 
R  plate (7). 
R  (c) Release the temperature sensor (1) from the brake subassembly 
R  (8). 
R  (d) Put a blanking cap in the temperature sensor housing. 
R  (5) Post SIL 32-0106 
R  (a) Disconnect the sensor assembly end (5) from the retainer 
R  subassembly (6) as follows: 
R  - unbend the ends of the clip (9). 
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM LANDING GEAR 起落架8(28)