- replace the EGIU-2 (22XU2).
**ON A/C 063-099, 106-149, 153-199, 206-299, 301-399,
A. If the test confirms the fault:
- do a check of the status of the C/B - APU GEN/EGIU2/115VAC (23XS).
(1) If it is open:
- close it.
(a) If it trips:
- do a check and repair the wiring between the pin AB/1D of the EGIU2 (22XU2) and the pin 9 of the module 29XN..
「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 238
201-299, 301-399, Aug 01/05 CES
(b) If it does not trip:
- do a check for continuity of the wiring between the circuit breaker (23XS) and the pin 9 of the module 29XN. (Ref. ASM 24-23/01).
(2) If the fault continues:
- replace the EGIU-2 (22XU2).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
B. Do this test to make sure that the systems operates correctly:
-------------------------------------------------------------------------------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. In the APU GEN box:
- the normal electrical parameters come into view.
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 electrical circuits supplied from the APU (Ref. AMM TASK 24-41-00-862-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-22-00∞∞∞∞∞∞∞∞∞∞Page 239
201-299, 301-399, Aug 01/05 CES
R **ON A/C ALL
TASK 24-22-00-810-814
Failure of the EMER ELEC PWR/GEN1 LINE Pushbutton Switch Circuit
1. Possible Causes
_______________
- P/BSW-EMER ELEC PWR/SMOKE DRILL (13XU)
- RELAY (20XU)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from Engine 1(2) AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the Engine 1(2)
AMM 31-60-00-860-001 EIS Start Procedure
AMM 33-10-00-000-002 Removal of the Bulbs and the Body of a Pushbutton
Switch in the Cockpit
AMM 33-10-00-400-002 Installation of the Bulbs and the Body of a
Pushbutton Switch in the Cockpit
AMM 71-00-00-710-003 Engine Automatic Start
AMM 71-00-00-710-028 Engine Shutdown
ASM 24-22/02
3. Fault Confirmation
__________________
A. Job Set-up
(1) Push the ELEC/GEN 1 pushbutton switch (3XU1).
(2) 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).
(3) Start the engine 1 (Ref. AMM TASK 71-00-00-710-003).
「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 240
Aug 01/05 CES
B. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel:
- push the ELEC key to get the ELEC page.
2. On the EMER ELEC PWR section of overhead panel 21VU:
- release and push the GEN 1 LINE pushbutton switch (13XU).
4. Fault Isolation
_______________On the upper ECAM DU:
- the EMER GEN 1 LINE OFF message comesinto view.
If on the upper ECAM DU:
- the EMER GEN 1 LINE OFF message goesout of view, stop the troubleshooting.
If on the upper ECAM DU:
- the EMER GEN 1 LINE OFF message stays in view, continue the trouble shooting (refer to the fault isolation which follows). 中國航空網 m.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(144)
