ABNORMAL
PROCEDURES
AIRPLANE
FLIGHT
MANUAL
4-16 ANAC APPROVED
Page 12 code 01 REVISION 7
AFM-1912
(Continued from the previous page)
If a go around is required, proceed as a normal go around limiting the
airspeed to 175 KIAS.
NOTE: As asymmetric thrust may be required to help controlling the
airplane, maximum thrust on both engines may not be
possible.
RUDDER 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 rudder button one
time.
If the RUDDER FAULT message persists and is associated with the
RUDDER LIMITER FAIL message, reset (push in, then out) the flight
controls mode rudder button once again.
If the RUDDER FAULT message persists, the following relevant items
will be inoperative:
− Yaw Damper.
− Turn Coordination.
RUDDER LIMITER FAILURE
Rudder position limiter is inoperative and rudder authority in flight
is 30°.
CAUTION:
• DO NOT APPLY ABRUPT PEDAL COMMANDS.
• DO NOT APPLY FULL RUDDER DEFLECTION.
SLAT-FLAP LEVER DISAGREE
Return the slat/flap lever to previous position and then use it as
required.