EasyManua.ls Logo

Embraer EMB145 - Page 426

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...
EMERGENCY
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-11
Page
2
Code
03
REVISION 40
AOM-145/1114
CONTINUED FROM PREVIOUS PAGE
EMERGENCY EVACUATION Procedure..................... AS REQUIRED
WARNING:
DO NOT ATTEMPT TO RESTART ENGINE.
IF IN ICING CONDITIONS, REFER TO SINGLE
ENGINE OR SINGLE BLEED OPERATION IN ICING
CONDITIONS PROCEDURE.
NOTE: - If in flight below 9700 ft, the air conditioning pack valves may
close automatically. The APU may be used as pneumatic
source by closing the remaining engine bleed valve.
- Engine will not shutdown with the START/STOP Selector
unless associated Thrust Lever is first moved to IDLE. If
STOP is selected before Thrust Lever is retarded to IDLE,
momentarily cycle START/STOP Selector to RUN and back
to STOP.
ENGINE LOW N1
EICAS WARNING: E1 (2) LOW N1
LIGHT: Master Warning
Do not takeoff.

Other manuals for Embraer EMB145

Related product manuals