Embraer EMB145 Operation Manual page 511

AILERON ARTIFICIAL FEEL INOPERATIVE
CONDITION: Control Wheel inputs become light and do not center by
itself.
Airspeed........................................................................ BELOW
Do not make sudden and large aileron inputs.
RUDDER ARTIFICIAL FEEL INOPERATIVE
CONDITION: Rudder pedals become extremely light and do not
center by themselves. Yaw trim does not operate
properly,
condition.
Rudder System 2 .......................................................... OFF
If the failure persists:
Rudder System 1..................................................... OFF
RUDDER MECHANICAL
REVERSION MODE Procedure......................... APPLY
ASYMMETRIC RUDDER OPERATION
CONDITION: Rudder pedals require more effort to be moved to one
side than the other. Also, the rudder and yaw trim
commands provide different results for both sides.
Rudder System 2 .......................................................... OFF
If the failure persists:
Rudder System 2..................................................... ON
Land at the nearest suitable airport.
The remainder of the flight should be made with both rudder systems
operational, which provides better rudder performance than in
mechanical reversion mode.
REVISION 40
AIRPLANE
OPERATIONS
MANUAL
although its
200 KIAS
pictorial indicates
1-03-53
ABNORMAL
PROCEDURES
normal
Page Code
7 03