- ELEC DC BUS2 FAULT
and if, on the lower ECAM DU:
- the amber DC 2 indication comes into view
- the line between DC 2 and DC BAT buses goes out of view
- the DC ESS bus is supplied by the ESS TR: . replace the CNTOR-DC NORM BUS 2 SWITCHING (1PC2) (Ref. AMM TASK 24-35-55-000-001) and (Ref. AMM TASK 24-35-55-400-001).
「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 ∞∞24-60-00∞∞∞∞∞∞∞∞∞∞Page 206
Feb 01/02 CES (1) If the fault continues:
- do a check and repair the wiring between: . the circuit breaker (14PC) and the pin B/3 of the contactor (1PC2), through the contactors (5PU2, 1PC1, 4PC) . the pin B/5 of the contactor (1PC2) and the ground (Ref. ASM 24-35/02).
R C. Do the test given in para. 3.
TASK 24-60-00-810-806 Unwanted Warning from the DC 1 Busbar
1. Possible Causes
_______________
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power AMM 31-60-00-860-001 EIS Start Procedure ASM 24-61/01 ASM 31-54/08
3. Fault Confirmation
__________________
A. Job Set-up
(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).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU EIS/SDAC1 AND 2/BUS1/28VDC 14WV P04 125VU 101PP/SPLY 1PN1 CD01
C. Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel: On the upper ECAM display unit:
- push the ELEC key to get the ELEC - the DC BUS1 FAULT warning comes into
page. view. On the lower ECAM display unit:
- the normal configuration comes into view with the DC 1 busbar shown in amber.
4. Fault Isolation
_______________
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
A. If the test confirms the fault:
- do a check and repair the wiring: . between the 28VDC BUS 1 (101PP) and the first branch point, the EIS/SDAC1 & 2/BUS1/28VDC circuit breaker (14WV) included, . then between the 28VDC BUS 1 (101PP) and the pin E of the TR1 contactor (5PU1), the 101PP SPLY circuit breaker (1PN1) included (Ref. ASM 31-54/08) and (Ref. ASM 24-61/01).
R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
A. If the test confirms the fault:
- do a check and repair the wiring: . between the 28VDC BUS 1 (101PP) and the first branch point, the EIS/SDAC1 & 2/BUS1/28VDC circuit breaker (14WV) included, . then between the 28VDC BUS 1 (101PP) and the pin 10 of the module 13PN, the 101PP SPLY circuit breaker (1PN1) included (Ref. ASM 31-54/08) and (Ref. ASM 24-61/01).
**ON A/C ALL
B. Do this test to make sure that the system operates correctly:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel: On the lower ECAM display unit:
- push the ELEC key to get the ELEC - the normal configuration comes into page. view.
「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 ∞∞24-60-00∞∞∞∞∞∞∞∞∞∞Page 209
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 3(143)
