Embraer 190 - Pitch Trim Failure (Embraer 195 Models); Rudder Failure

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-16
REVISION 7 code 01 Page 11
AFM-1912
PITCH TRIM FAILURE
(EMBRAER 195 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.
Reset (push in, then out) the pitch trim system 1 and 2 cutout buttons.
Actuate pitch trim switches.
If pitch trim is not moving upon command, push in the pitch trim
system 1 and 2 cutout buttons. No more pitch trim is available.
For landing configuration, set slat/flap to 5 and set
V
REF FULL
+ 20 KIAS.
CAUTION:
MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 1.42.
Establish landing configuration early.
If a go around is required, maintain slat/flap 5 and
V
REF FULL
+ 20 KIAS until the acceleration altitude is reached.
RUDDER FAILURE
LAND AT THE NEAREST SUITABLE AIRPORT.
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.
Relevant Inoperative Items:
− Yaw Trim.
− Yaw Damper.
− Turn Coordination.
For landing configuration, set slat/flap to full and set V
REF FULL
.
CAUTION:
AVOID LANDING WITH CROSSWIND COMPONENTS
ABOVE 10 KT.
(Continued on the next page)