Embraer EMB145, Operation Manual

Page: 426 / 2662

EMERGENCY
PROCEDURES AIRPLANE
OPERATIONS
MANUAL
1-03-11
Page
2
Code
03 REVISION 40 A
O
M-145/1
114
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.