Embraer 190 - Flap (Slat) Failure (Embraer 195 Models)

ABNORMAL
PROCEDURES
AIRPLANE
FLIGHT
MANUAL
4-16 ANAC APPROVED
Page 8 code 01 REVISION 7
AFM-1912
FLAP (SLAT) FAILURE
(EMBRAER 195 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.
FLAP/SLAT FAIL LANDING TABLE
SLAT
FLAP
0 3 FULL
V
REF
(KIAS)
V
REF FULL
+ 60 V
REF FULL
+ 50 V
REF FULL
+ 50
Ldg Coef
0
1.80 1.75 1.80
V
REF
(KIAS)
V
REF FULL
+ 35 V
REF FULL
+ 35 V
REF FULL
+ 35
Ldg Coef
1
1.50 1.50 1.55
V
REF
(KIAS)
V
REF FULL
+ 30 V
REF FULL
+ 25 V
REF FULL
+ 25
Ldg Coef
2
1.40 1.38 1.40
V
REF
(KIAS)
V
REF FULL
+ 20 V
REF FULL
+ 10
Ldg Coef
3, 4 and 5
1.30 1.20
V
REF
(KIAS)
V
REF FULL
+ 5 V
REF FULL
Ldg Coef
FULL
NOT
USABLE
1.08 NOT APPLICABLE
(Continued on the next page)