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Embraer 175 - DUAL ENGINE FAILURE

Embraer 175
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EMERGENCY
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-01 ANAC APPROVED
Page 4 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
DUAL ENGINE FAILURE
φAirspeed ......................................................................250 KIAS MIN
φRAT Manual Deploy Lever ..........................................PULL
LAND AT THE NEAREST SUITABLE AIRPORT.
Start the APU, set the emergency lights to off and the thrust levers to
idle.
If both engines were restarted via autorelight, reset (push in, then push
out) the flight controls mode buttons (spoilers, elevators and rudder).
For landing configuration, arm the emergency lights, push in the
ground proximity flap override button, set slat/flap to 3 and set
V
REF FULL
+ 15 KIAS.
CAUTION:
MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 1.31.
If one or no engine were restarted via auto relight, check the airstart
envelope, set the fuel crossfeed selector knob to low 1 and, for the
inoperative engine(s), set the start/stop selector(s) to stop, the
ignition(s) to override and then, the start/stop selector(s) to start, then
run.
If the dual engine failure condition persists, for landing
configuration, arm the emergency lights, set slat/flap to 3 and set
V
REF FULL
+ 20 KIAS or 130 KIAS (whichever is higher) and
accomplish the Forced Landing or Ditching Procedure.
If the dual engine failure condition does not persist, reset (push in,
then push out) the flight controls mode buttons (spoilers, elevators
and rudder) and, after the engine(s) stabilized at idle, set ignition(s)
to auto and balance fuel. During descent, set the landing data, the
approach aids and the altimeters. For landing configuration, arm the
emergency lights, push in the ground proximity flap override button,
set landing gear down, set slat/flap to 3 and set V
REF FULL
+ 20 KIAS.
CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED
LANDING DISTANCE BY 2.10.
If a go around is required, maintain slat/flap to 3 and V
REF FULL
+
2
0 KIAS until the acceleration altitude is reached.

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