Embraer 190 - Pitch Trim Failure (Embraer 190 Models)

ABNORMAL
PROCEDURES
AIRPLANE
FLIGHT
MANUAL
4-16 ANAC APPROVED
Page 10 code 01 REVISION 7
AFM-1912
PITCH TRIM 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.
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
+ 15 KIAS.
CAUTION:
MULTIPLY THE FULL FLAPS UNFACTORED
LANDING DISTANCE BY 1.29.
Establish landing configuration early.
If a go around is required, maintain slat/flap 5 and
V
REF FULL
+ 15 KIAS until the acceleration altitude is reached.