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TASK 77-30-00-810-811
Failure of the TRF Vibration Sensor on Engine 1
1. Possible Causes
_______________
- EVMU (2EV)
- wiring from the EVMU (2EV) to the TRF vibration sensor (4003EV)
- SENSOR-TRF VIB (4003EV)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 77-31-30-000-002 Removal of the Turbine Rear Frame Vibration Sensor AMM 77-31-30-400-002 Installation of the Turbine Rear Frame Vibration Sensor AMM 77-32-34-000-042 Removal of the Engine Vibration Monitoring Unit (EVMU) AMM 77-32-34-400-042 Installation of the Engine Vibration Monitoring Unit (EVMU)
R AMM 77-32-34-710-040 Operational Check of EVMU through CFDS AMM 77-32-34-860-041 Change the configuration of the Accelerometer ASM 77-32/02
3. Fault Confirmation
__________________
A. Test Do the operational test of the Engine Vibration Monitoring Unit (EVMU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 77-32-34-710-040).
4. Fault Isolation
_______________
A. If the test gives the maintenance message ENG1 SECOND ACCEL:
- do a check of the wiring from the EVMU (2EV) to the TRF vibration sensor (4003EV) pins AA/1C, 2D to pins AA/2, 3 (Ref. ASM 77-32/02).
(1) If there is no continuity:
- repair the above wiring.
(2) If there is continuity:
- reconfigure the accelerometer to get the data from the No. 1 bearing vibration sensor (Ref. AMM TASK 77-32-34-860-041)
- if necessary, replace the SENSOR-TRF VIB (4003EV), (Ref. AMM TASK 77-31-30-000-002) and (Ref. AMM TASK 77-31-30-400-002).
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E F 『 E C F M E E E E 56 E E E (3) If the fault continues:
- replace the EVMU (2EV), (Ref. AMM TASK 77-32-34-000-042) and (Ref. AMM TASK 77-32-34-400-042).
B. Do the test given in Para. 3.A.
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TASK 77-30-00-810-812
Failure of the TRF Vibration Sensor on Engine 2
1. Possible Causes
_______________
- EVMU (2EV)
- wiring from the EVMU (2EV) to the TRF vibration sensor (4003EV)
- SENSOR-TRF VIB (4000EV)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 77-31-30-000-002 Removal of the Turbine Rear Frame Vibration Sensor AMM 77-31-30-400-002 Installation of the Turbine Rear Frame Vibration Sensor AMM 77-32-34-000-042 Removal of the Engine Vibration Monitoring Unit (EVMU) AMM 77-32-34-400-042 Installation of the Engine Vibration Monitoring Unit (EVMU)
R AMM 77-32-34-710-040 Operational Check of EVMU through CFDS AMM 77-32-34-860-041 Change the configuration of the Accelerometer ASM 77-32/02
3. Fault Confirmation
__________________
A. Test Do the operational test of the Engine Vibration Monitoring Unit (EVMU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 77-32-34-710-040).
4. Fault Isolation
_______________
A. If the test gives the maintenance message ENG 2 SECOND ACCEL:
- do a check of the wiring from the EVMU (2EV) to the TRF vibration sensor (4003EV) pins AB/1C, 2D to pins AA/2, 3 (Ref. ASM 77-32/02).
(1) If there is no continuity:
- repair the above wiring.
(2) If there is continuity:
- reconfigure the accelerometer to get the data from the No. 1 bearing vibration sensor (Ref. AMM TASK 77-32-34-860-041)
- if necessary, replace the SENSOR-TRF VIB (4000EV), (Ref. AMM TASK 77-31-30-000-002) and (Ref. AMM TASK 77-31-30-400-002).
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E F 『 E C F M E E E E 56 E E E (3) If the fault continues:
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 發(fā)動(dòng)機(jī)指示(190)
