EasyManua.ls Logo

Embraer EMB145 - Page 1919

Embraer EMB145
2662 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
POWERPLANT
AIRPLANE
O
PERATIONS
MANUAL
2-10-50
Page
18
Code
01
REVISION 41
Copyright © by Embraer. Refer to cover page for details.
AOM
-
145/1114
ENGINE SHUTDOWN
Normal engine shutdown, through the Start/Stop Knob, is managed by
the FADEC, which commands the engine fuel solenoid valve to close.
The normal sequence only occurs with the thrust levers positioned at
Idle. Thrust levers should be positioned at IDLE before the Start/Stop
Knob is positioned at Stop.
A shutdown sequence is also performed whenever N2 is below 54%.
NOTE: The Engine Fire Extinguishing Handle, when actuated, also
shuts the engine down by closing the respective fuel shutoff
valve, interrupting fuel supply from the wing tanks.