- The IGN indication and the starter valve symbols come into view.
NOTE : Ignore the warnings that occur
____ during the procedure that follows.
- The ON legend of this pushbuttonswitch comes on.
On the engine 1(2):
- Make sure that the two igniter plugsmake a noise. On the lower ECAM display unit, on the ENGINE page:
- The A and B indications come into view.
On the engine 1(2):
- Make sure that only one igniter plug makes a noise.
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5. On the REAR C/B PNL 121VU: - Open the circuit breaker 3JH1 (3JH2).
6. On the OVERHEAD C/B PNL 49VU: - Close the circuit breaker 1JH.
R 7. On the REAR C/B PNL 121VU: - Close the circuit breaker 3JH1 (3JH2).
R R R 8. On the ENG PNL 115VU: - Set the ENG/MASTER 1(2) control switch to OFF.
R R R R R R 9. On the OVERHEAD CTL & IND CTL 22VU: - Release the ENG/MAN START/1(2) pushbutton switch.
10. On the ENG PNL 115VU: - Set the ENG/MODE/CRANK/NORM/IGN START selector switch to NORM.
On the engine 1(2):
- Make sure that there is no noise fromthe two igniter plugs.
On the engine 1(2):
- Make sure that only one igniter plug makes a noise.
On the engine 1(2):
- Make sure that the two igniter plugsmake a noise.
On the engine 1(2):
- Make sure that there is no noise from the two igniter plugs.
- The ON legend of this pushbutton switch goes off. On the lower ECAM display unit, on the ENGINE page:
- The A and B indications go out of view.
NOTE : The ECU stays electrically supplied for 5 minutes after you set:
____
- the ENG/MASTER 1(2) lever to OFF.
- The ENG/MODE/CRANK/NORM/IGN START rotary selector to NORM.
NOTE : The WARNING messages that appears during this procedure can be
____ cleared by an ON/OFF switching of the ENG/MASTER 1(2) control switch.
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________ Subtask 74-00-00-860-054
A. Put the aircraft back to its initial configuration.
(1) On the MAINTENANCE PNL 50VU:
(a) Push the ENG / FADEC GND PWR / 1(2) pushbutton switch. The ON legend goes off.
(2) Do the EIS stop procedure: (Ref. TASK 31-60-00-860-002). Subtask 74-00-00-862-051
B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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TASK 74-00-00-710-044
Operational Test of Continuous Ignition Selection in Case of EIU Failure or Engine Anti-Ice Selection
1. Reason for the Job
__________________
To do an operational test of the continuous ignition logics in case of EIU
failure or selection of engine anti-ice.
NOTE : This procedure applies only for aircraft that have the AIDS.
____
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
71-00-00-710-003 Engine Automatic Start
71-00-00-710-028 Engine Shutdown
3. Job Set-up
__________
Subtask 74-00-00-861-052
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