AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-16
REVISION 7 code 01 Page 5
AFM-1912
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
the 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. The following relevant items will be
inoperative:
− AOA Limit. − Autopilot.
− Auto Configuration Trim. − Elevator Thrust Compensation.
ELEVATOR LH (RH) FAILURE
(EMBRAER 190 MODELS)
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 1.29.
(Continued on the next page)
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