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.
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