(2) If the circuit breaker is open:
- close it.
(a) If it trips:
- do a check of the wiring for a short to ground between respectively the pins A/2, B/2, C/2 of the circuit breaker (2PU2) and the pins 22, 23, 24 of the module 20XX (Ref. ASM 24-32/01).
1 If the wiring is not correct:
_ - repair it.
2 If the wiring is correct:
_ - replace the C/B-TR2 SPLY (2PU2).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-60-00∞∞∞∞∞∞∞∞∞∞Page 216
Aug 01/05 CESR **ON A/C ALL
C. Do the test given in Para. 3. to make sure that no warning message comes into view on the upper ECAM display unit, and that the cabin lights come on when the related pushbutton switches are pushed.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
TASK 24-60-00-810-809
Failure of the DC BUS TIE (Loss of the Connection between the DC 2 Bus and the
DC BAT Bus)
1. Possible Causes
_______________
- CNTOR-DC NORM BUS 2 SWITCHING (1PC2)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 24-32-00-710-001 Operational Test of the DC Generation Switching
AMM 24-35-55-000-001 Removal of the Contactor (1PC1, 1PC2)
AMM 24-35-55-400-001 Installation of the Contactor (1PC1, 1PC2)
ASM 24-35/02
3. Fault Confirmation
__________________
A. Test Do the operational test of the DC generation switching (Ref. AMM TASK 24-32-00-710-001).
4. Fault Isolation
_______________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R 122VU ELEC/CNTOR/DC BUS/TIE 1/FAULT 14PC U24
B. If the fault symptom is identified by these warnings on the upper ECAM DU:
- ELEC TR1 FAULT
- ELEC DC BUS1 FAULT
and if, on the lower ECAM DU:
- the amber DC 1 and DC BAT indications come into view
- the line between DC 2 and DC BAT buses goes out of view
- the green line between DC 1 and DC BAT buses come on
- 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 218
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 DC NORM BUS2 switching 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 24-60-00-810-810
Loss of the 28VDC SHED ESS Bus 801PP
1. Possible Causes
_______________
- CNTOR-DC SHED ESS BUS (8PH)
- RELAY-B HYD PUMP CTL (21XE)
- RELAY - STAT INV CTL (6XB)
- EMER/SHED/CNTOR/SPLY (1PH)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 23-71-00-710-001 Operational Test of the CVR and the CVR Channel Recording 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 24-62-55-000-001 Removal of the DC Shed Essential Bus Contactor (8PH) AMM 24-62-55-400-001 Installation of the DC Shed Essential Bus Contactor
(8PH) AMM 31-60-00-860-001 EIS Start Procedure ASM 24-62/01 AWM 24-62-02
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 3(146)
