- replace the P/BSW-ELEC/GEN 1 (3XU1).
(b) If the contacts operate correctly:
- replace the RELAY-GLC 1 AUX CTL (4XU1). 1 If the fault continues:
_
- do a check and repair the wiring for an open circuit between pin A/7A of the GCU 1 and the ground (Ref. ASM 24-22/02).
「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 : 001-049, 051-099, 101-149, 151-199, ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 245
201-299, 301-399, Aug 01/05 CES B. When you replace a component or repair the wiring:
- do the subsequent flight before you do the check to make sure that the problem related to this fault symptom is repaired. If the upper ECAM DU gives the GEN 1 FAULT warning, continue the trouble shooting.
「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 : 001-049, 051-099, 101-149, 151-199, ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 246
201-299, 301-399, Aug 01/05 CES
TASK 24-00-00-810-820
GEN 2 FAULT Warning without Associated Message on the ECAM
1. Possible Causes
_______________
- GCU-2 (1XU2)
- P/BSW-ELEC/GEN 2 (3XU2)
- RELAY-GLC 2 AUX CTL (4XU2)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 24-22-34-000-001 Removal of the GCU-1(2) (1XU1, 1XU2)
AMM 24-22-34-400-001 Installation of the GCU-1(2) (1XU1, 1XU2)
ASM 24-22/03
3. Fault Confirmation
__________________
A. Test
Not applicable, no confirmation test is necessary.
4. Fault Isolation
_______________
A. If the fault symptom is identified by the upper ECAM DU warning GEN 2 FAULT:
- replace the GCU-2 (1XU2) (Ref. AMM TASK 24-22-34-000-001) and (Ref. AMM TASK 24-22-34-400-001).
(1) If the fault continues:
- do a check of the contacts of the ELEC/GEN 2 pushbutton switch (3XU2) for correct operation (Ref. ASM 24-22/03).
(a) If the contacts do not operate correctly:
- replace the P/BSW-ELEC/GEN 2 (3XU2).
(b) If the contacts operate correctly:
- replace the RELAY-GLC 2 AUX CTL (4XU2). 1 If the fault continues:
_
- do a check and repair the wiring for an open circuit between pin A/7A of the GCU 2 and the ground (Ref. ASM 24-22/03).
「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 : 001-049, 051-099, 101-149, 151-199, ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 247
201-299, 301-399, Aug 01/05 CES B. When you replace a component or repair the wiring:
- do the subsequent flight before you do the check to make sure that the problem related to this fault symptom is repaired. If the upper ECAM DU gives the GEN 2 FAULT warning, continue the trouble shooting.
「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 : 001-049, 051-099, 101-149, 151-199, ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 248
201-299, 301-399, Aug 01/05 CES
R **ON A/C 106-149, 229-299, 303-399, 401-499,
R TASK 24-00-00-810-821
R Failure of the Oil Temperature Sensors of the IDG 1 without Overtemperature R Detection R 1. Possible Causes
_______________
R - IDG (4000XU) R - GCU-1 (1XU1) R - wiring
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 12-13-24-612-041 R R AMM 24-21-00-210-046 R R AMM 24-21-00-920-040 R R AMM 24-21-51-000-040 R R AMM 24-21-51-400-040 R R AMM 24-22-34-000-001 R AMM 24-22-34-400-001 R AMM 24-41-00-740-002 R ASM 24-21/01
R 3. Fault Confirmation
__________________
R A. Test IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a level Check Check of the Oil Level and Oil-Filter Differential-Pressure Indicator (DPI) Drain IDG Oil System, Discard Filter Element(s) and Replenish Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) Installation of the Integrated Drive Generator -IDG 1(2),(4000XU) Removal of the GCU-1(2) (1XU1, 1XU2) Installation of the GCU-1(2) (1XU1, 1XU2) Operational Check of GAPCU via CFDS
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 1(92)
