R 6. On the ELEC panel 35VU:
R - Push the AC ESS FEED pushbutton
R switch.
R
R
R
R
R
R 5. Close-up
________
R Subtask 24-30-00-860-055
-
The FAULT legend of the AC ESS FEED pushbutton switch goes off.
-
The ALTN legend of the AC ESS FEED pushbutton switch comes on.
On the lower ECAM DU, on the ELEC page:
-A green bar comes into view between the AC2 and AC ESS busbars. This shows that the AC2 busbar energizes the AC ESS busbar,
-
The green bar between the AC1 and AC ESS busbars goes out of view.
On the ELEC panel 35VU:
-
The ALTN legend of the AC ESS FEED pushbutton switch goes off.
On the ELEC page:
-
The green bar between the AC2 and AC ESS busbars goes out of view.
-
The green bar between the AC1 and AC ESS busbars comes into view.
R A. Put the aircraft back to its initial configuration.
R (1) Do the EIS stop procedure
R (Ref. TASK 31-60-00-860-002).
R (2) De-energize the aircraft electrical circuits
R (Ref. TASK 24-41-00-862-002).
R TASK 24-30-00-440-002 R Reactivation of the Transformer Rectifier TR2 (1PU2) R 1. Reason for the Job
__________________ R Self Explanatory R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-41-00-861-002 R R 24-41-00-862-002 R R 31-60-00-860-001 R 31-60-00-860-002 R TSM 24-30-00-810-802
R 3. Job Set-up__________
R Subtask 24-30-00-860-056 Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power EIS Start Procedure EIS Stop Procedure Failure of the TR2 or TR2 Contactor or Related Wiring
R A. Aircraft Maintenance Configuration
R (1) Energize the aircraft electrical circuits
R (Ref. TASK 24-41-00-861-002).
R (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
R (Ref. TASK 31-60-00-860-001). R 4. Procedure
_________
R Subtask 24-30-00-440-050
R A. Do the trouble shooting of the TR2 (Ref. TSM TASK 24-30-00-810-802).
R 5. Close-up________
R Subtask 24-30-00-860-057
R A. Put the aircraft back to its initial configuration.
R (1) Do the EIS stop procedure
R (Ref. TASK 31-60-00-860-002).
R (2) De-energize the aircraft electrical circuits
R (Ref. TASK 24-41-00-862-002).
DC GENERATION - ADJUSTMENT/TEST
_______________________________
TASK 24-30-00-710-001
Operational Test of the Emergency Generation System with One Normal Transformer Rectifier (TR) Failed
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
1. Reason for the Job
__________________
CSM/G Test with one normal TR Failed.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platforms 1.8 m (5 ft. 11 in.)
B. 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 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 71-00-00-710-003 Engine Automatic Start 71-00-00-710-028 Engine Shutdown
3. Job Set-up
__________
Subtask 24-30-00-860-050
A. Aircraft Maintenance 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 HYD/FUEL panel 40VU, make sure that the OFF legend of the BLUE ELEC PUMP pushbutton switch is OFF.
Subtask 24-30-00-010-052
B. Get access to the Avionics Compartment
(1) Put the access platforms at the access doors 812 and 822.
(2) Open the access doors 812 and 822.
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2(28)
