Embraer 175 - Takeoff

AIRPLANE
FLIGHT
MANUAL
NORMAL
PROCEDURES
ANAC APPROVED 3-16
REVISION 15 code 01 Page 1
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
TAKEOFF
Thrust Levers........................................................... TOGA
Engine Parameters.................................................. MONITOR
NOTE: During takeoff roll, after checking thrust levers to TOGA, check
N1 equal to N1 target and green ATTCS indication presented
on EICAS if ATTCS ON is selected in MCDU.
At V
R
rotate the airplane following the flight director pitch angle.
In case of flight director is inoperative, rotate the airplane according to
following schedule:
− For airplanes Pre-Mod. SB 170-31-0019:
FLAPS POSITION
1 2 4
PITCH ANGLE
11° 10° 12°
− For airplanes Post-Mod. SB 170-31-0019 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.
With positive rate of climb:
Landing Gear...................................................... UP
Minimum Airspeed.............................................. V
2
+ 10