4-18
Shutdown
Shutdown
4-18-01
WARNING
IN CASE OF ENGINE FIRE, DO THE
Note
−
Allow ITT to stabilize at least two minutes at ground idle
−
Monitor compressor deceleration after shutdown for possible engine damage
−
In case of an unusual amount of smoke from the engine exhaust after
shutdown, allow ITT to stabilize and then conduct a
.
Note
If a shutdown is commanded with indicated T1 temperature at or above
approximately 23 °C, the EPECS will command a momentary (15 second) dry
motoring cycle during the shutdown sequence, indicated by
STARTER
on the
PFD engine window and
DRY MOTORING
on the CAS window.
A dry motoring run at shutdown can always be aborted by setting the Master
Power switch to EMERGENCY OFF.
1.
Power Control Lever...................
IDLE DETENT
2.
Parking Brake.............................
SET / PEDALS PUSH
3.
ICE PROTECTION switches.......
OFF
4.
Inertial Separator........................
OPEN, if operating on unprepared
surface
5.
Feather Inhibit switch (if
installed)......................................
PUSH and HOLD (if desired, refer to
note)
Note
After 9 consecutive engine shutdowns using the propeller feather inhibit function,
a normal engine shutdown must be performed (refer to Section 2, Limitations,
Power Plant Limitations,
6.
Engine switch..............................
OFF
Note
The optional Feather Inhibit function activates when the Feather Inhibit switch is
pushed and held while at the same time the Engine switch is set to OFF. Once the
Feather Inhibit status message shows on the CAS, the pilot can release the
Feather Inhibit switch and the function will continue to execute automatically.
Continued on next page
Section 4 - Normal Procedures (EASA Approved)
Shutdown
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 4-18-1
12-C-A15-30-0418-00A-131A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
