3. Fault Confirmation
__________________
A. Job Set-up
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
(3) Start the APU:
- GTCP 36-300 (Ref. AMM TASK 49-00-00-860-003)
or
- APS 3200 (Ref. AMM TASK 49-00-00-860-005)
or
- 131-9(A) (Ref. AMM TASK 49-00-00-860-008).
B. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: On the upper ECAM DU:
- push the ELEC key to get the - the APU GEN OVERLOAD message comes ELEC page. into view.
2. On the ELEC panel 35VU: If on the upper ECAM DU:
- release the GALLEY pushbutton - the APU GEN OVERLOAD message goes out
switch (2XA). of view, stop the trouble shooting. If on the upper ECAM DU:
- the APU GEN OVERLOAD message stays in view, continue the trouble shooting (refer to the fault isolation which follows).
「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 ∞∞24-23-00∞∞∞∞∞∞∞∞∞∞Page 207
Aug 01/05R
CES
4. Fault Isolation
_______________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
**ON A/C 001-049, 051-060, 101-102, 201-201,
122VU ELEC/GALLEY/CTL 1XA S26
122VU ELEC/GALLEY/FAULT/LT CTL 8XA S25
**ON A/C ALL
122VU ELEC/GCU/1 2XU1 T26
R **ON A/C 061-099, 103-149, 151-199, 202-299, 301-399, 401-499,
122VU ELEC/GALY & CAB/CTL 1XA S26
122VU ELEC/GALY & CAB/FAULT/LT CTL 8XA S25
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
B. If the test confirms the fault:
- open the circuit breakers 8XA and 1XA
- replace the P/BSW-ELEC/GALLEY (2XA) (Ref. AMM TASK 33-10-00-000-002) and (Ref. AMM TASK 33-10-00-400-002)
- close the circuit breakers 8XA and 1XA.
(1) If the fault continues:
- remove the APU GCU (1XS) (Ref. AMM TASK 24-23-34-000-001)
- close the circuit breaker 2XU1.
(a) If the fault does not continue:
- install a new GCU-APU (1XS) (Ref. AMM TASK 24-23-34-400-001).
(b) If the fault continues:
- open the circuit breakers 8XA and 1XA
- disconnect the connector of the diode module 1162VD (Ref. IPC 25710104)
- close the circuit breakers 8XA and 1XA.
1 If the fault does not continue:
_ - open the circuit breakers 8XA and 1XA
- replace the diode module 1162VD (Ref. IPC 25710104)
- install the APU GCU (1XS) (Ref. AMM TASK 24-23-34-400-001)
- close the circuit breakers 8XA and 1XA
「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 ∞∞24-23-00∞∞∞∞∞∞∞∞∞∞Page 208
Aug 01/05 CES 2 If the fault continues:
_
- replace the EGIU-2 (22XU2) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
a If the fault does not continue:
_ - open the circuit breakers 8XA and 1XA
- connect the connector of the diode module 1162VD (Ref. IPC 25710104)
- install the APU GCU (1XS) (Ref. AMM TASK 24-23-34-400-001)
- close the circuit breakers 8XA and 1XA.
b If the fault continues:
_ - open the circuit breakers 8XA and 1XA
- do a check and repair the wiring between: . the pin A/11 of the diode module 1162VD and the pin AA/13B of the APU GCU (1XS) . the pin A/11 of the diode module 1162VD and the pin AB/10A of the EGIU2 (22XU2) . the pin A/11 and the pin A/10 of the diode module 1162VD
- connect the connector of the diode module 1162VD (Ref. IPC 25710104)
- install the APU GCU (1XS) (Ref. AMM TASK 24-23-34-400-001)
- close the circuit breakers 8XA and 1XA.
R **ON A/C 401-499,
R B. If the test confirms the fault:
R - open the circuit breakers 8XA and 1XA
R - replace the P/BSW-ELEC/GALLEY (2XA)
R - close the circuit breakers 8XA and 1XA.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 3(9)
