Embraer EMB145 - Page 428

EMERGENCY
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-11
Page
4
Code
03
REVISION 40
(Pages 4A to 4B deleted)
AOM-145/1114
DUAL ENGINE FAILURE
EICAS WARNING: ENG 1-2 OUT
LIGHT: Master Warning
Airspeed ........................................................................ MINIMUM
260 KIAS
Oxygen Mask (if required)............................................. DON
Altitude .......................................................................... MAX 25000 ft
ENGINE AIRSTART Procedure.................................... ACCOMPLISH
CAUTION:
IF APU HAS BEEN USED TO START THE ENGINES, DO
NOT ALTERNATE THE FADECS AFTER START.
NOTE: If APU is not available, only equipment supplied by the
Essential DC Bus 1 and 2 will be available. Engine windmilling
should drive engine driven pumps and supply hydraulic
pressure.
If neither engine can be restarted:
FORCED LANDING Procedure ............................... ACCOMPLISH
ENGINE OIL LOW PRESSURE
EICAS WARNING: E1 (2) OIL LOW PRESS (may be presented)
LIGHT: Master Warning
INDICATION: Oil pressure indication may be red.
Oil Pressure Indication.................................................. CHECK
If flight conditions permit, reduce N2 below 88% and monitor oil
temperature and oil quantity indication.
Monitor oil pressure for the remainder of the flight. If oil pressure is in
the red range:
Associated Thrust Lever .......................................... IDLE
If oil pressure is still in the red range:
PRECAUTIONARY ENGINE
SHUTDOWN Procedure .......................................... ACCOMPLISH