Cessna 172N - Page 73

CESSNA
MODEL
172N
STATL
SPEEDS
CONDITIONS:
Power Off
NOTES:
1.
Maximum
altitude loss during
a stall
recovery
may be
as
much
as 180
feet.
2.
KIAS
values are approximate.
SECTION 5
PERFORMANCE
frlOST
REARW ARD
CENTER OF
GRAVITY
,VIOSI
FORWARD
CENTER OF GRAVIIY
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF
BANK
oo
300
450
600
KIAS
KCAS KIAS
KCAS KIAS KCAS KIAS KCAS
2300
UP
loo
400
42
38
36
50
47
M
45
40
38
54
51
47
50
45
43
59
56
52
59
54
51
71
66
62
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF
BANK
go
3oo
450
600
KIAS
KCAS
KIAS KCAS KIAS KCAS KIAS
KCAS
2300
UP
100
400
47
44
41
53
51
47
51
47
M
57
55
51
56
52
49
63
61
56
66
62
58
75
72
66
Figure
5-3.
Stall Speeds
5- 11