(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
B. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: On the upper ECAM display unit:
- push the ELEC key to get the - the ELEC DC EMER CONFIG warning comes
ELEC page. into view. On the lower ECAM display unit:
- the amber DC 1, DC 2 and DC ESS indications come on
- the amber TR 1, TR 2 and ESS TR indications come on with the related parameters.
「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 230
Aug 01/00R CES
4. Fault Isolation
_______________
A. If the test confirms the fault:
- make sure that no tool or other item has been forgotten in the panel 120VU.
(1) If the result of the inspection is correct:
- do a check and repair the internal wiring of the different parts of the panel 120VU for short to ground between the break connectors and successively the circuit breakers and other components.
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).
「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 231
Aug 01/00R
CES
TASK 24-60-00-810-814
Failure of the DC Emergency Generation
1. Possible Causes
_______________
- CNTOR-ESS TR (3PE)
- TR-ESS (1PE)
- CNTOR-AC ESS BUS SWITCHING (15XE)
- wiring
- C/B-ESS TR CNTOR CTL (5PE)
- C/B-ESS TR SPLY (4PE)
- C/B-AC ESS/BUS/EMER/CNTOR/SPLY (15PC)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 24-24-55-000-002 Removal of the AC ESS BUS Contactor (15XE)
AMM 24-24-55-400-002 Installation of the AC ESS BUS Contactor (15XE)
AMM 24-34-51-000-001 Removal of the Essential Transformer Rectifier (1PE)
AMM 24-34-51-400-001 Installation of the Essential Transformer Rectifier
(1PE) AMM 24-34-55-000-001 Removal of the Essential TR Contactor (3PE) AMM 24-34-55-400-001 Installation of the Essential TR Contactor (3PE) 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
AMM 31-60-00-860-002 EIS Stop Procedure
ASM 24-24/02
ASM 24-34/01
ASM 24-35/01
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
106VU AC ESS/BUS/EMER/CNTOR/SPLY 15PC C08
106VU ESS TR/CNTOR/CTL 5PE C02 R 106VU ESS TR/SPLY 4PE C01 R
123VU TR1/SPLY 2PU1 AB10
「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 232
中國航空網 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 3(150)
