AIRPLANE
FLIGHT
EMERGENCY
PROCEDURES
ANAC APPROVED 4-01
REVISION 15 code 01 Page 9
Copyright © by Embraer. Refer to cover page for details.
JAMMED RUDDER PEDALS
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: Use assymetric thrust for directional control. For landing
configuration set slat/flap to full and set V
REF FULL
.
CAUTION: DURING LANDING, A CROSSWIND COMPONENT
GREATER THAN 10 KT MUST BE AVOIDED.
Before landing, the pilot not flying must press and hold the steering
disconnect switch. Use assymetric thrust until nosewheel touchdown.
After nosewheel touchdown, press and hold the nosewheel steering
handle, release the steering disconnect switch, reduce the thrust levers
and use differential braking as required.
CAUTION:
DO NOT RELEASE THE NOSEWHEEL STEERING
HANDLE UNTIL THE AIRPLANE IS COMPLETELY
STOPPED.
If a go around is required, proceed as a normal go around limiting the
airspeed to 175 KIAS.
NOTE: As assymetric thrust may be required to help controlling the
airplane, maximum thrust on both engines may not be
possible.