Embraer 175 - Flap;Slat Fail Landing Table with Shaker Anticipated

ABNORMAL
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-16 ANAC APPROVED
Page 6 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
(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
1.85 1.83 1.82
V
REF
(KIAS)
V
REF FULL
+ 40 V
REF FULL
+ 40 V
REF FULL
+ 40
Ldg Coef
1
1.62 1.60 1.60
V
REF
(KIAS)
V
REF FULL
+ 30 V
REF FULL
+ 25 V
REF FULL
+ 25
Ldg Coef
2
1.38 1.55 1.57
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