Embraer 190 - Flap (Slat) Failure (Embraer 190 Models)

ABNORMAL
PROCEDURES
AIRPLANE
FLIGHT
MANUAL
4-16 ANAC APPROVED
Page 6 code 01 REVISION 7
AFM-1912
(Continued from the previous page)
If a go around is required, maintain slat/flap 5 and V
REF FULL
+ 15 KIAS
until the acceleration altitude is reached.
ELEVATOR LH (RH) FAILURE
(EMBRAER 195 MODELS)
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 less elevator control authority and slower response,
especially during landing flare.
For landing configuration, set slat/flap to 5 and set V
REF FULL
+ 15 KIAS.
Apply brakes only after the nose landing gear touches down.
CAUTION:
MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 1.40.
If a go around is required, maintain slat/flap 5 and V
REF FULL
+ 15 KIAS
until the acceleration altitude is reached.
FLAP (SLAT) FAILURE
(EMBRAER 190 MODELS)
Cycle the slat/flap lever (up to three cycles may be attempted).
If the FLAP (SLAT) FAIL message persists, use the position indicated
on the EICAS as a reference to select landing data presented on the
tables below. If there is no flap (slat) indication in the EICAS, use the
more conservative position to enter the table.
Limit Bank angle to 20° maximum. If applicable, push in the Gnd Prox
Flap Ovrd Button.
If a go around is required, maintain the Slat/Flap lever in the selected
position and set the V
REF
presented in the table until the level off.
(Continued on the next page)