Embraer 190 - Page 260

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-16
REVISION 7 code 01 Page 7
AFM-1912
(Continued from the previous page)
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
1.90 1.77 1.81
V
REF
(KIAS)
V
REF FULL
+ 35 V
REF FULL
+ 35 V
REF FULL
+ 35
Ldg Coef
1
1.52 1.56 1.58
V
REF
(KIAS)
V
REF FULL
+ 30 V
REF FULL
+ 25 V
REF FULL
+ 25
Ldg Coef
2
1.44 1.39 1.41
V
REF
(KIAS)
V
REF FULL
+ 20 V
REF FULL
+ 10
Ldg Coef
3, 4 and 5
1.35 1.22
V
REF
(KIAS)
V
REF FULL
+ 5 V
REF FULL
Ldg Coef
FULL
NOT
USABLE
1.08 NOT APPLICABLE
FLAP/SLAT FAIL LANDING TABLE WITH SHAKER ANTICIPATED
SLAT
FLAP
0 3 FULL
V
REF
(KIAS)
V
REF FULL
+ 60 V
REF FULL
+ 60 V
REF FULL
+ 60
Ldg Coef
0
1.90 1.95 1.99
V
REF
(KIAS)
V
REF FULL
+ 40 V
REF FULL
+ 40 V
REF FULL
+ 40
Ldg Coef
1
1.60 1.63 1.66
V
REF
(KIAS)
V
REF FULL
+ 30 V
REF FULL
+ 30 V
REF FULL
+ 30
Ldg Coef
2
1.44 1.47 1.49
V
REF
(KIAS)
V
REF FULL
+ 20 V
REF FULL
+ 15
Ldg Coef
3, 4 and 5
1.35 1.29
V
REF
(KIAS)
V
REF FULL
+ 5 V
REF FULL
Ldg Coef
FULL
NOT
USABLE
1.08 NOT APPLICABLE