Lower ECAM Display Unit - ELEC Page
Figure 006 (SHEET 2)
1EFF : ALL 1 24-00-00 Page 37
1 1 Aug 01/05
1 1
1CES 1
ELECTRICAL POWER - GENERAL - ADJUSTMENT/TEST
____________________________________________ TASK 24-00-00-710-003 Integrity Test of the Electrical Power
1.
Reason for the Job
__________________
To ensure aircraft safety after maintenance work on the wiring.
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-004 Procedure to Get Access to the SYSTEM
REPORT/TEST/ELEC Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________ Subtask 24-00-00-860-056
A. Aircraft Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(3)
On the ECAM control panel, push the ELEC key (on the lower ECAM DU, the ELEC page comes into view).
(4)
On the MCDU, get the system REPORT/TEST/ELEC page (Ref. TASK 31-32-00-860-004).
Subtask 24-00-00-865-061
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU SDAC/1 AND 2/28VDC/ESS BUS 106VU DC BUS/1 AND 2/MONG 12WV 68WV F05C03
**ON A/C 001-049, 051-060, 101-102, 201-201,
122VU ELEC/GALLEY/GND/FLT/LOGIC 7XA S24
**ON A/C ALL
122VU ELEC/BUS/2XP/CTL 122VU ELEC/AC/BUS1/CTL 122VU ELEC/CNTOR/DC/BUS/TIE1 122VU ELEC/EXT PWR/LT CLT/NOT IN/USE 122VU ELEC/TR2/MONG 122VU ELEC/TR1/MONG 17XN2 17XN1 9PC 6XG 3PU2 3PU1 V27V25W25X30X26X25
R **ON A/C 061-099, 103-149, 151-199, 202-299, 301-399, 401-499,
122VU ELEC/GALY & CAB/GND/FLT/LOGIC 7XA S24
**ON A/C ALL
123VU TR1/SPLY 123VU TR2/214XP/SPLY 123VU AC ESS/BUS ON/BUS 1 123VU AC ESS/BUS ON/BUS 2 124VU TR2/CNTOR/SPLY 125VU TR1/CNTOR/SPLY 2PU1 2PU2 1XC 2XC 4PU2 4PU1 AB10AB04AC12AC01BC01CF01
4. Procedure
_________ Subtask 24-00-00-710-050
A. Energization of the Aircraft with the Batteries 1 and 2
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ELEC control panel 35VU: - push the AC ESS FEED, BUS TIE and GALLEY pushbutton switches - release the EXT POWER pushbutton switch - push the BAT 1 and BAT 2 pushbutton switches. On the ELEC control panel 35VU:- the AVAIL legend of the EXT POWERpushbutton switch comes on- the battery voltmeters must show avoltage of 28 volts.
2. On the EMER ELEC PWR section of the panel 21VU: - open the guard, push and hold the EMER GEN TEST pushbutton switch. The PFD and the upper ECAM DU imagescome into view.
R 3. On the ECAM control panel: - push and hold the ELEC key. On the upper ECAM DU, on the ELEC page:- the STAT INV indications come into view (115V, 400Hz) - the BAT indications come into view
R R (28V, 20A) (values are given for information) .
Subtask 24-00-00-710-051
B. Ground Service Configuration
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the control panel 2000VU: In the right avionics compartment:
-set the MAINT BUS switch to ON - the TR2 operates.
2. On the panel 122VU: In the right avionics compartment
- open then close the circuit - the TR2 does not operate.
breaker 6XG.
Subtask 24-00-00-710-052
C. Loss of the Busbars 1XP and 2XP
-------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------- 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM ELECTRICAL POWER 电源1(33)
