Embraer 175 - ELEVATOR LH (RH) FAILURE

ABNORMAL
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-16 ANAC APPROVED
Page 4 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
AFM
-
1385
ANGLE OF ATTACK LIMIT FAILURE
Avoid sideslipping the airplane.
NOTE: The stick shaker remains operative.
ELEVATOR THRUST COMPENSATOR
FAILURE
Compensate manually any pitch tendency following thrust variations.
ELEVATOR FAULT
NOTE: If the SPOILER FAULT message is also displayed, accomplish
th
e Spoiler Fault Procedure prior to this procedure.
Reset (push in, then out) the flight controls mode elevators button one
time.
If the ELEVATOR FAULT message persists, accomplish the Angle of
Attack Limit Failure Procedure.
ELEVATOR LH (RH) FAILURE
If the failure occurs above 175 KIAS, the current airspeed is the
maximum speed for the remainder of the flight.
If the failure occurs below 175 KIAS, the maximum speed for the
remainder of the flight is 175 KIAS.
NOTE: Expect less elevator control authority and slower response,
especially during landing flare.
For landing configuration, set slat/flap to 5 and set V
REF FULL
+ 15 KIAS.
Apply brakes only after the nose landing gear touches down.
CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 1.40.
If a go around is required, set slat/flap to 4 and maintain
V
REF FULL
+ 15 KIAS until the acceleration altitude is reached.