Embraer 175 - FUEL LEAK; JAMMED CONTROL COLUMN (PITCH)

AIRPLANE
FLIGHT
MANUAL
EMERGENCY
PROCEDURES
ANAC APPROVED 4-01
REVISION 15 code 01 Page 7
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
FUEL LEAK
LAND AT THE NEAREST SUITABLE AIRPORT.
Set the fuel crossfeed selector to off and identify the affected fuel tank.
Use asymmetric thrust to improve or maintain wing fuel balance to
counteract the effect of the suspected wing fuel leak.
If fuel leak is identified on the right side tank, set APU to off.
If fuel leak is identified on the left side tank, use APU as required.
JAMMED CONTROL COLUMN (PITCH)
φE
levator 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 pitch rates and authority.
Accomplish the AOA Limit Failure Procedure.
For landing configuration set slat/flap to 5 and set V
REF FULL
+ 15 KIAS.
CAUTION: 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.