Embraer 175 - JAMMED CONTROL WHEEL (ROLL)

EMERGENCY
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-01 ANAC APPROVED
Page 8 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
JAMMED CONTROL WHEEL (ROLL)
φAileron Disconnection Handle..................................... PULL
Identify the unrestricted control column.
If the failure occurs above 175 KIAS, the current airspeed is the
maximum speed for the remainder of the flight.
If the failure occurs below 175 KIAS, the maximum speed for the
remainder of the flight is 175 KIAS.
NOTE: - Expect lower roll rates.
- Avoid abrupt and large aileron inputs.
- Maintain bank angle below 25°.
- Rudder may be used to help controlling the airplane.
- Do not accomplish the Spoiler Fault Procedure.
For landing configuration set slat/flap to 5 and set V
REF FULL
+ 15 KIAS.
C
AUTION: • DURING LANDING, A CROSSWIND COMPONENT
GREATER THAN 10 KT MUST BE AVOIDED.
• MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 1.40.
If a go around is required, maintain V
REF FULL
+ 15 KIAS (limited to
175 KIAS) until the acceleration altitude is reached.