Shutdown of the Engine for an Emergency [PW11]

TASK 71-00-00-860-815-A
Shutdown of the Engine for an Emergency

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.

1. Reason for the Job
Use this procedure to shutdown the engine during an emergency.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	COVER - PROTECTION

B. 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)
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 71-00-00-860-817-A	Motor the Engine (Dry Method)
Shutdown of the Engine for an Emergency

3. Job Set-up
Subtask 71-00-00-869-341-A ** ON A/C NOT FOR ALL

A. Not Applicable

4. Procedure
Subtask 71-00-00-860-182-A ** ON A/C NOT FOR ALL

A. Shutdown of the Engine for an Emergency
(1) Quickly and immediately move the Engine 1 or Engine 2 thrust lever to the IDLE position.
(2) If conditions permit, operate the engine at IDLE for ten minutes before you shut down the engine. Otherwise, go to Step 4.A.(3).

NOTE: An emergency shutdown is a shutdown from power levels higher than IDLE. Use this emergency shutdown procedure only for emergency conditions which do not let you use a normal shutdown procedure.

NOTE: A hot shutdown is considered to be shutting down the engine that was operated above 70% N1 for more than one minute in preceding 20 minutes of operation.

(3) On the center pedestal, on ENG panel 115VU:
(a) Set the ENG/MASTER 1(2) control switch to OFF.

NOTE: This will stop the fuel supply to the engine.

(4) If the engine has a tail pipe fire, dry-motor the engine with the starter when N2 is less than 20% on the engine display panel, until the fire goes out. Do not obey the starter time limits if the engine has a tailpipe fire (Ref. AMM TASK 71-00-00-860-817).
(5) If the engine shutdown was a hot shutdown, do the steps that follow:
(a) In less than five minutes after the emergency shutdown (or when N2 is less than 20%), dry-motor the engine as follows (Ref. AMM TASK 71-00-00-860-817).
1 Dry motor the engine but do not exceed the extended starter duty cycle of 15 minutes maximum continuous cranking.
(6) Set the EXT LT/BEACON switch to OFF position.
(7) Maintenance action is due.
(8) Examine the assembly for foreign objects, damage and correct assembly.
(9) Installation of protection covers

CAUTION: INSTALL PROTECTION COVERS ON ALL THE OPENINGS IMMEDIATELY TO PREVENT DAMAGE TO THE ENGINE.

(a) Make sure that you install COVER - PROTECTION as necessary to prevent damage to the engine.

5. Close-up
Subtask 71-00-00-860-264-A ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) On HYD/FUEL panel 40VU:
(a) Release all the FUEL/PUMPS pushbutton switches (the OFF legends of these pushbutton switches come on).
(2) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 12:57:04 UTC