Embraer 175 - FLAP (SLAT) FAILURE

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-16
REVISION 15 code 01 Page 5
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
FLAP (SLAT) FAILURE
Return to the previous position and after reselect the desired position.
This can be attempted up to two times.
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
1.85 1.74 1.72
V
REF
(KIAS)
V
REF FULL
+ 35 V
REF FULL
+ 35
V
REF FULL
+ 35
Ldg Coef
1
1.53 1.51 1.50
V
REF
(KIAS)
V
REF FULL
+ 30 V
REF FULL
+ 25 V
REF FULL
+ 20
Ldg Coef
2
1.38 1.55 1.28
V
REF
(KIAS)
V
REF FULL
+ 15 V
REF FULL
+ 10
Ldg Coef
3, 4 and 5
1.31 1.29
V
REF
(KIAS)
V
REF FULL
+ 5 V
REF FULL
Ldg Coef
FULL
NOT
USABLE
1.06 NOT APPLICABLE
(Continues on the next page)