(3) If the wiring is not correct:
- repair it.
(4) If the wiring is correct:
- Replace the engine IDG1 (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040).
(5) If the fault continues:
- do a check and repair the wiring between respectively the pins A1, A6, A7, A8 of the IDG1 and the pins B/13D, B/13A, B/13B, B/13C of the GCU1.
**ON A/C 063-099, 106-149, 153-199, 206-299, 301-399,
A. If the fault symptom is identified by the maintenance message CHECK BTC1 PIN D, E, F, R, P, N SHORT TO GROUND and by the warning GEN1 FAULT on the upper ECAM display unit:
- do a check of the feeder for short to ground between respectively: . the pins 4, 5, 6 of the module 30XN1 and the main bus . the pins 10, 11, 12 of the module 30XN1 and the pins 10, 11, 12 of the module 29XN (Ref. ASM 24-22/02)
(1) If the wiring is not correct:
- repair it.
(2) If the wiring is correct:
- do a check of the IDG1 feeders for intermittent short to ground between respectively the pins A/T1, B/T2, C/T3 of the IDG1 and the pins 1, 2, 3 of the module 30XN1.
(3) If the wiring is not correct:
- repair it.
(4) If the wiring is correct:
- Replace the engine IDG1 (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page 214
201-299, 301-399, Aug 01/05 CES (5) If the fault continues:
- do a check and repair the wiring between respectively the pins A1, A6, A7, A8 of the IDG1 and the pins B/13D, B/13A, B/13B, B/13C of the GCU1.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
B. Do this operational test to make sure that the system operates correctly.
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
(2) On the panel 35VU:
- push, release and push again the GEN1 pushbutton switch (3XU1).
(3) Do the operational test of the GPCU (Ref. AMM TASK 24-41-00-740-002).
(4) Start the engine 1 (Ref. AMM TASK 71-00-00-710-003).
(5) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel: On the lower ECAM display unit:
- push the ELEC key to get the ELEC - the correct electrical parameters of
page. GEN1 are shown and AC1 busbar is supplied by GEN1.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) Stop the engine 1 (Ref. AMM TASK 71-00-00-710-028).
(2) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page 215
201-299, 301-399, Aug 01/05 CES
TASK 24-20-00-810-807
Accidental Disconnection of the IDG1
1. Possible Causes
_______________
- RELAY-IDG1 DISC CTL (3XT)
- wiring
- P/BSW-ELEC/IDG1 (5XT)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 24-21-00-710-040 Operational Test of the IDG Disconnect and Reconnect (Reset) Function - Engine Static AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
AMM 71-00-00-710-003 Engine Automatic Start
AMM 71-00-00-710-028 Engine Shutdown
ASM 24-21/01
3. Fault Confirmation
__________________
A. Test
Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
A. If the fault symptom is identified by the CFDS message IDG1 DISCONNECTED and the warning ELEC GEN1 FAULT on the upper ECAM display unit:
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 1(101)
