(5) If the fault continues:
- do a check for 115 VAC at the pins B,C,D and E,F,G, and I,J,K at the related GALLEYS.
(a) If there is no 115 VAC :
- do a check of the related GALLEY PWR RELAY and replace it if necessary.
(6) If the fault continues:
- do a check and repair the wiring between the related: GALLEY pins B,C,D or E,F,G or I,J,K and the related CB, GALLEY pins A or H or L and the related GND (Ref. ASM 24-56/01).
B. If the white indicator light FAULT in PBSW 2XA does not come on, but there is a fault in the galley equipment:
- do a check of the PBSW 2XA and replace it if necessary.
(1) If the fault continues:
- do a check and repair the wiring between: CB 1XA and PBSW 2XA connector A/C3 (Ref. ASM 24-56/01).
C. Do the test as given in Para. 3.A. to check the correct operation (no maintenance message is shown).
GALLEY SUPPLY - TASK SUPPORTING DATA
____________________________________
Power Supply - Block Diagram
Figure 301
「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 ∞∞24-56-00∞∞∞∞∞∞∞∞∞∞Page 302
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DC ELECTRICAL LOAD DISTRIBUTION - FAULT ISOLATION PROCEDURES
____________________________________________________________
TASK 24-60-00-810-801
Unwanted Warning from the DC ESS SHED Busbar
1. Possible Causes
_______________
- 8PH
- 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) ASM 24-62/01
3. Fault Confirmation
__________________
A. Job Set-up
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
B. Test Do the operational test of the CVR and the CVR channel recording (test of the CVR only) (Ref. AMM TASK 23-71-00-710-001).
(1) If the test is correct:
- 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 ELEC page comes into view. page.
On the upper ECAM display unit:
- the ELEC DC ESS BUS SHED warning comes into view.
4. Fault Isolation
_______________
A. If the test confirms the fault:
- replace the 8PH (Ref. AMM TASK 24-62-55-000-001) and (Ref. AMM TASK 24-62-55-400-001).
(1) If the fault continues:
- do a check and repair the wiring between: . the pin B/21 of the contactor (8PH) and the first branch point . the pin B/19 of the contactor (8PH) and the ground (Ref. ASM 24-62/01).
B. Do this test to make sure that the system operates correctly:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel:
- push the ELEC key to get the ELEC page.
5. Close-up
________
On the lower ECAM display unit:
- the ELEC page comes into view.
On the upper ECAM display unit:
- no warning comes into view.
A. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-60-00∞∞∞∞∞∞∞∞∞∞Page 202
Feb 01/98 CES
TASK 24-60-00-810-803
Loss of the DC Busbars
1. Possible Causes
_______________
- TR-1 (1PU1)
- TR-2 (1PU2)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 3(141)
