Embraer EMB145 - Page 506

ABNORMAL
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-53
Page
2
Code
03
REVISION 40
AOM-145/1114
AILERON SYSTEM INOPERATIVE
EICAS CAUTION: AIL SYS 1 (2) INOP
LIGHT: Master Caution
Associated Aileron System ........................................... OFF
Airspeed ........................................................................ MAXIMUM
250 KIAS
If the remaining system fails:
Remaining Aileron System ...................................... OFF
Quick Disconnect Button ......................................... PRESS
Aileron is operating under mechanical reversion mode. Expect greater
aileron control force. If required, both pilots should act together to
control airplane. Avoid landing at airports with anticipated turbulence
or crosswind. Perform a long final approach.
Approach and landing configuration:
Landing Gear ........................................................... DOWN
Flaps ........................................................................ 22°
Airspeed................................................................... V
REF 45
+
30 KIAS
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING
DISTANCE FOR FLAPS 45° BY 1.85.
RUDDER OVERBOOST
EICAS CAUTION: RUDDER OVERBOOST
LIGHT: Master Caution
Rudder System 2 .......................................................... OFF
Check that only RUDDER 2 SYS INOP message is presented on
EICAS.
If the message disappears:
Continue flight with rudder system 2 off.
Below 135 KIAS:
Rudder System 2 ................................................ ON
If message remains:
Rudder System 2 ..................................................... ON
Rudder System 1 ..................................................... OFF
Check that only RUDDER 1 SYS INOP message is presented on
EICAS.
Continue flight with the rudder system 1 off.
Below 135 KIAS:
Rudder System 1 ................................................ ON