Embraer EMB145, Operation Manual

Page: 511 / 2662

AIRPLANE
OPERATIONS
MANUAL
ABNORMAL
PROCEDURES
REVISION 40
1-03-53
Page
7
Code
03
A
O
M-145/1
114
AILERON ARTIFICIAL FEEL INOPERATIVE
CONDITION: Control Wheel inputs become light and do not center by
itself.
Airspeed........................................................................ BELOW
200 KIAS
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, although its pictorial indicates normal
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.