Start Abort [CFML]

TASK 71-00-00-860-830-A
Start Abort

CAUTION: BE PREPARED TO DRY MOTOR THE ENGINE IF THE EGT DOES NOT DECREASE. DRY MOTORING THE ENGINE CAN PREVENT A FIRE AFTER SHUTDOWN.

1. Reason for the Job
Use this procedure when it is necessary to stop an engine start in the manual mode in case on ECAM indication requiring an engine shut down.
2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)

3. Job Set-up
Subtask 71-00-00-869-370-A

A. Not Applicable

4. Procedure
Subtask 71-00-00-710-255-A

A. Stop the engine.

CAUTION: MAKE SURE THAT THE ENG/MASTER 1(2) CONTROL SWITCH IS FULLY ENGAGED IN THE OFF DETENT AFTER SHUTDOWN.

(1) Set the ENG/MASTER 1(2) control switch to OFF.
(2) Monitor the EGT, N2 and fuel flow during the shutdown to confirm the fuel shutoff.

CAUTION: BE PREPARED TO DRY MOTOR THE ENGINE WITH THE STARTER IF THERE IS A POST-SHUTDOWN FIRE INDICATION. ENGINE DAMAGE CAN BE CAUSED.

(a) Make sure that the EGT and N2 rpm decrease when the fuel is shut off. If a steady decrease in the EGT does not occur after the shutdown, do a dry-motoring until the fire is extinguished.

NOTE: After the engine shutdown is completed, and the rotation is fully stopped, the EGT will normally slowly increase. This is caused by a normal temperature soak-back.

(3) Release the ENG/MAN START 1(2) pushbutton switch, ON legend goes off.
(4) Put the ENG/MODE/CRANK/NORM/START selector switch to NORM or CRANK if some fuel has been injected.
(5) On the HYD/FUEL panel 40VU:
(a) Release all the FUEL/PUMPS pushbutton switches (the OFF legends of these pushbutton switches come on).
(6) On the overhead control and indicating panel 25VU:
(a) Set the EXT LT/BEACON switch to OFF.
(7) If necessary, install the covers that you removed at engine start on the TAT, AOA and PITOT probes.

NOTE: Do not install the probe covers immediately after the engine shutdown.

Subtask 71-00-00-862-103-A

B. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.02 06:33:13 UTC