Embraer 190 - Page 191

AIRPLANE
FLIGHT
MANUAL
EMERGENCY
PROCEDURES
ANAC APPROVED 4-01
REVISION 3 code 01 Page 15
AFM
-
1912
TAKEOFF WITH ENGINE FAILURE AT OR
ABOVE V
1
(EMBRAER 195 MODELS)
φAt V
R
rotate the airplane following the flight director guidance.
φIn case of flight director is inoperative rotate the airplane according
the following schedule:
- For airplanes Pre-Mod. SB 190-31-0009:
FLAPS POSITION
1 2
3
4
PITCH ANGLE
11° 11° 9° 11°
- For airplanes Post-Mod. SB 190-31-0009 or equipped with an
equivalent modification factory incorporated, rotate the airplane
according to the takeoff pitch angle displayed on TAKEOFF page 3/3
on the MCDU.
φWith positive climb:
φLanding Gear......................................................... UP
φAirspeed................................................................. MIN V
2
Maintain V
2
m
inimum up to the acceleration altitude. At the
acceleration altitude, select slat/flap up according to the flap retraction
speed reference.
Accelerate the airplane to the final segment speed (V
FS
) and set the
engine thrust rate to continuous.
After retracting flaps, accomplish the Engine 1 (2) Failure Procedure.