Embraer 190 - Page 262

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-16
REVISION 7 code 01 Page 9
AFM-1912
(Continued from the previous page)
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
1.80 1.82 1.85
V
REF
(KIAS)
V
REF FULL
+ 40 V
REF FULL
+ 40 V
REF FULL
+ 40
Ldg Coef
1
1.53 1.55 1.60
V
REF
(KIAS)
V
REF FULL
+ 30 V
REF FULL
+ 30 V
REF FULL
+ 30
Ldg Coef
2
1.40 1.42 1.44
V
REF
(KIAS)
V
REF FULL
+ 20 V
REF FULL
+ 15
Ldg Coef
3, 4 and 5
1.30 1.25
V
REF
(KIAS)
V
REF FULL
+ 5 V
REF FULL
Ldg Coef
FULL
NOT
USABLE
1.08 NOT APPLICABLE
FLIGHT CONTROL BIT EXPIRED
Do not takeoff.
FLIGHT CONTROL NO DISPATCH
Do not takeoff.