「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 ∞∞24-22-00∞∞∞∞∞∞∞∞∞∞Page 223
Aug 01/05 CES (b) If the circuit breaker (23XS) is closed:
- do a check and repair the wiring between the circuit breaker APU GEN/EGIU2/115VAC (23XS) and the pin AB/1D of the EGIU2 (22XU2) (Ref. ASM 24-23/01).
1 If the fault continues:
_
- do a check and repair the wiring between the circuit breaker APU GEN/EGIU2/115VAC (23XS) and the pin A/D of the APU GLC (3XS) (Ref. ASM 24-23/01).
(2) If the fault continues:
- do a check and repair the wiring (Ref. ASM 31-54/03) between: . the pin B/13A of the EGIU2 (22XU2) and the pin B/10J of the SDAC1 (1WV1) . the pin B/13B of the EGIU2 (22XU2) and the pin B/10K of the SDAC1 (1WV1) . the pin B/13C of the EGIU2 (22XU2) and the pin B/10J of the SDAC2 (1WV2) . the pin B/13D of the EGIU2 (22XU2) and the pin B/10K of the SDAC2 (1WV2)
D. If the test confirms the fault:
- replace the EGIU-2 (22XU2) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
(1) If the fault continues:
- do a check of the wiring between: . the pin A/2B of the APU GCU (1XS) and the pin B/9D of the EGIU2 (22XU2), . the pin A/2C of the APU GCU (1XS) and the pin B/9C of the EGIU2 (22XU2). Then make sure that the ground wire is correctly connected to the pin B/10D of the EGIU2 (22XU2) (Ref. ASM 24-23/02).
(2) If the fault continues:
- replace the GCU-APU (1XS) (Ref. AMM TASK 24-23-34-000-001) and (Ref. AMM TASK 24-23-34-400-001).
(3) If the fault continues:
- do a check and repair the wiring (Ref. ASM 31-54/03) between: . the pin B/13A of the EGIU2 (22XU2) and the pin B/10J of the SDAC1 (1WV1) . the pin B/13B of the EGIU2 (22XU2) and the pin B/10K of the SDAC1 (1WV1) . the pin B/13C of the EGIU2 (22XU2) and the pin B/10J of the SDAC2 (1WV2) . the pin B/13D of the EGIU2 (22XU2) and the pin B/10K of the SDAC2 (1WV2)
「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, ∞∞24-22-00∞∞∞∞∞∞∞∞∞∞Page 224
201-299, 301-399, Aug 01/05 CES
R **ON A/C 401-499,
R B. If the test confirms the fault:
R - replace the GAPCU (24XG) (Ref. AMM TASK 24-41-34-000-001) and (Ref. AMM
R TASK 24-41-34-400-001).
R (1) If the fault continues:
R - replace the GEN-APU (8XS) (Ref. AMM TASK 24-23-51-000-001) and
R (Ref. AMM TASK 24-23-51-400-001).
R C. If the test confirms the fault:
R - replace the GAPCU (24XG) (Ref. AMM TASK 24-41-34-000-001) and (Ref. AMM
R TASK 24-41-34-400-001).
R (1) If the fault continues:
R - replace the GEN-APU (8XS) (Ref. AMM TASK 24-23-51-000-001) and
R (Ref. AMM TASK 24-23-51-400-001).
R (a) If the fault continues:
R - do a check and repair the wiring (Ref. ASM 31-54/03) between:
R . the pin A/8J of the GAPCU (24XG) and the pins B/10J, E/10A of
R the SDAC 1 (1WV1)
R . the pin A/8H of the GAPCU (24XG) and the pins B/10K, E/10B of
R the SDAC 1 (1WV1)
R . the pin A/8F of the GAPCU (24XG) and the pins B/10J, E/10A of
R the SDAC 2 (1WV2)
R . the pin A/7F of the GAPCU (24XG) and the pins B/10K, E/10B of
R the SDAC 2 (1WV2).
R D. If the test confirms the fault:
R - do a check and repair the wiring (Ref. ASM 31-54/03) between:
R . the pin A/8J of the GAPCU (24XG) and the pins B/10J, E/10A of the
R SDAC 1 (1WV1)
R . the pin A/8H of the GAPCU (24XG) and the pins B/10K, E/10B of the
R SDAC 1 (1WV1)
R . the pin A/8F of the GAPCU (24XG) and the pins B/10J, E/10A of the
R SDAC 2 (1WV2)
R . the pin A/7F of the GAPCU (24XG) and the pins B/10K, E/10B of the
R SDAC 2 (1WV2).
R **ON A/C ALL
E. Do this test to make sure that the system operates correctly:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel: On the lower ECAM DU:
- push the ELEC key to get the ELEC - the ELEC page comes into view.
page. In the APU GEN box:
- the normal electrical parameters come into view. 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 2(139)
