- replace the SENSOR, BRK TEMP, WHEEL 4 (6GW) (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 (6GW) (Ref. AMM TASK 32-47-15-400-001)
- replace the MONITORING UNIT-BRK TEMP, R (2GW) (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 (2GW) to the sensor (6GW) pins A/A, C (Ref. ASM 32-47/01).
(4) If the fault continues:
- do a check and repair the wiring from the BTMU (2GW) to the BSCU (10GG) pin A/D to pin AB/10D (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 211
Aug 01/05R
CES
R **ON A/C 106-149, 221-299, 401-499,
B. If the test gives the maintenance message BRAKE TEMP SENSOR4(6GW)/BTMU(2GW): - on the brake 4 disconnect the connector of the brake temperature sensor
6GW (Ref. AMM TASK 32-47-15-000-001)
- on the connector of the brake temperature sensor 6GW, 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 generator, increase the voltage.
(1) If the related temperature indication increases on the WHEEL page
- replace the SENSOR, BRK TEMP, WHEEL 4 (6GW) (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 (6GW) (Ref. AMM TASK 32-47-15-400-001)
- replace the MONITORING UNIT-BRK TEMP, R (2GW) (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 (2GW) to the sensor (6GW) pins A/A, C (Ref. ASM 32-47/01).
(4) If the fault continues:
- do a check and repair the wiring from the BTMU (2GW) to the BSCU (10GG) pin A/D to pin AB/10D (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 212
Aug 01/05 CES
TASK 32-47-00-810-805
Loss of the Brake Temperature Monitoring on the Wheel 3 and 4
1. Possible Causes
_______________
- MONITORING UNIT-BRK TEMP, R1 (2GW)
- BSCU (10GG)
- wiring from the BTMU (2GW) pin A/A to the first terminal block
- wiring from the BTMU (2GW) to the BSCU (10GG)
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
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AMM 32-42-34-000-001 Removal of the Braking/Steering Control Unit (BSCU) (10GG) AMM 32-42-34-400-001 Installation of the Braking/Steering Control Unit (BSCU) (10GG)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 起落架 LANDING GEAR 2(74)
