- replace the SENSOR-BRK TEMP, WHEEL 1 (5GW) (Ref. AMM TASK 32-47-15-000-001) and (Ref. AMM TASK 32-47-15-400-001).
(2) If the related temperature indication does not increase on the WHEEL page:
- connect the connector of the brake temperature sensor (5GW) (Ref. AMM TASK 32-47-15-400-001)
- replace the MONITORING UNIT-BRK TEMP, L (3GW) (Ref. AMM TASK 32-47-18-000-001) and (Ref. AMM TASK 32-47-18-400-001).
(3) If the fault continues:
- do a check and repair the wiring from the BTMU (3GW) to the sensor (5GW) pins A/A, C (Ref. ASM 32-47/01).
(4) If the fault continues:
- do a check and repair the wiring from the BTMU (3GW) to the BSCU (10GG) pin A/C to pin AB/9C (Ref. ASM 32-47/01).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-47-00∞∞∞∞∞∞∞∞∞∞Page 202
May 01/05 CESR **ON A/C 106-149, 221-299, 401-499,
B. If the test gives the maintenance message BRAKE TEMP SENSOR1(5GW)/BTMU(3GW): - on the brake 1, disconnect the connector of the brake temperature
sensor 5GW (Ref. AMM TASK 32-47-15-000-001)
- on the connector of the brake temperature sensor 5GW, connect a DC Generator (0 to 50 mv) with the voltage adjusted to zero millivolt and a millivoltmeter with the polarity as follows: Terminal A: Negative. Terminal C: Positive.
- Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GW
- on the ECAM control panel, push the WHEEL key to get the WHEEL page - on the DC generators, increase the voltage.
(1) If the related temperature indication increases on the WHEEL page
- replace the SENSOR-BRK TEMP, WHEEL 1 (5GW) (Ref. AMM TASK 32-47-15-000-001) and (Ref. AMM TASK 32-47-15-400-001).
(2) If the related temperature indication does not increase on the WHEEL page:
- connect the connector of the brake temperature sensor (5GW) (Ref. AMM TASK 32-47-15-400-001)
- replace the MONITORING UNIT-BRK TEMP, L (3GW) (Ref. AMM TASK 32-47-18-000-001) and (Ref. AMM TASK 32-47-18-400-001).
(3) If the fault continues:
- do a check and repair the wiring from the BTMU (3GW) to the sensor (5GW) pins A/A, C (Ref. ASM 32-47/01).
(4) If the fault continues:
- do a check and repair the wiring from the BTMU (3GW) to the BSCU (10GG) pin A/C to pin AB/9C (Ref. ASM 32-47/01).
**ON A/C ALL
C. Do the test given in Para. 3.A. (Ref. AMM TASK 32-46-00-740-001).
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-47-00∞∞∞∞∞∞∞∞∞∞Page 203
Aug 01/05 CES TASK 32-47-00-810-802
Loss of the Brake Temperature Monitoring on the Wheel 2
1. Possible Causes
_______________
- MONITORING UNIT-BRK TEMP, L (3GW)
- SENSOR-BRK TEMP, WHEEL 2 (7GW)
- wiring from the BTMU (3GW) to the sensor (7GW) pins A/A, C
- wiring from the BTMU (3GW) to the BSCU (10GG)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific millivoltmeter
No specific DC Generator (0 to 50 mv)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power
AMM 31-60-00-860-001 EIS Start Procedure
AMM 32-46-00-740-001 BITE Test of the BSCU
AMM 32-47-15-000-001 Removal of the Brake Temperature Sensor
(4GW,5GW,6GW,7GW)
AMM 32-47-15-400-001 Installation of the Brake Temperature Sensor
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 起落架 LANDING GEAR 2(70)
