ABNORMAL
PROCEDURES
AIRPLANE
F
LIGHT
4-16 ANAC APPROVED
Page 10 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
STABILIZER LOCK FAULT
LAND AT THE NEAREST SUITABLE AIRPORT.
The Horizontal Stabilizer may have a drift rate up to 0.5 deg/min nose up
or nose down.
Use pitch trim as required.
CAUTION: DO NOT PRESS ANY PITCH TRIM SYSTEM CUTOUT
BUTTON.
AILERON RH (LH) FAILURE
On ground, do not takeoff.
In
flight:
Avoid abrupt and large aileron inputs and limit bank angle to 25°.
Establish landing configuration early. For landing configuration, set
slat/flap 5 and maintain V
REF FULL
+ 10 KIAS.
CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED
LANDING DISTANCE BY 1.30.
FLIGHT CONTROL FAULT
Do not takeoff.