(2)
In the cockpit, on the overhead panel 35VU, make sure that the GEN1
(2) pushbutton switch is released.
4. Procedure
_________ Subtask 24-27-00-710-050
A. Operational Test of the GEN FAULT Warning:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 35VU:
-push the GEN1(2) pushbutton switch.
2. On the panel 35VU:
-release the GEN1(2) pushbutton switch.
5. Close-up
________
Subtask 24-27-00-862-050On the panel 35VU:
-
the FAULT legend of the GEN1(2)pushbutton switch comes on.
On the panel 35VU:
-
the FAULT legend of the GEN1(2)pushbutton switch goes off,
-
the OFF legend of the GEN1(2) pushbutton switch comes on.
A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
TASK 24-27-00-710-002
Operational Test of the Automatic Galley Shedding
1. Reason for the Job
__________________
Make sure that the automatic galley shedding is operative when there are no more indications on the ECAM ELEC page.
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the APU 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the APU
3. Job Set-up
__________ Subtask 24-27-00-860-051
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits from the APU (Ref. TASK 24-41-00-861-002).
(2)
In the cockpit, on the overhead panel 35VU, make sure that the GALLEY pushbutton switch is pushed (the OFF legend is off).
(3)
In the forward and aft galleys, make sure that all the units operate.
1EFF : ALL 1 24-27-00Page 503 1 1 Feb 01/99R 1 1 1CES 1
Subtask 24-27-00-865-050
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
**ON A/C 001-049, 051-060, 101-102, 201-201,
122VU ELEC/GALLEY/CTL 1XA S26 122VU ELEC/GALLEY/FAULT/LT CTL 8XA S25 122VU ELEC/GALLEY/GND/FLT/LOGIC 7XA S24
R **ON A/C 061-099, 103-149, 151-199, 202-299, 301-399, 401-499,
122VU ELEC/GALY & CAB/CTL 1XA S26 122VU ELEC/GALY & CAB/FAULT/LT CTL 8XA S25 122VU ELEC/GALY & CAB/GND/FLT/LOGIC 7XA S24
**ON A/C ALL
4. Procedure
_________
Subtask 24-27-00-710-051
A. Operational Test of the Automatic Galley Sheeding:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 122VU: In the forward and aft galleys:
- open the circuit breaker 7XA. - make sure that only the secondary units operate.
5. Close-up
________
Subtask 24-27-00-862-051
A. De-energize the aircraft electrical circuits supplied from the APU. (Ref. TASK 24-41-00-862-002).
STATIC INVERTER (GENERATION) - DESCRIPTION AND OPERATION
________________________________________________________
1. General
_______
The 1000 VA nominal-power static inverter transforms the direct current
voltage from battery 1 into a single-phase 115 VAC/400 Hz alternating
current.
2. Component Location
__________________
(Ref. Fig. 001, 002)
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------2XB CNTOR-STAT INV 105VU 126 822 24-28-55 3XB STAT INV 126 822 24-28-51
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本文鏈接地址：A320飛機維護手冊 AMM ELECTRICAL POWER 電源2(16)
