Textron Cessna 172R - Page 162

SECTION
5
PERFORMANCE
CESSNA
MODEL
172R
STALL
SPEEDS
AT
2450
POUNDS
Conditions:
Power
Off
MOST
REARWARD
CENTER
OF
GRAVITY
FLAP
SETTING
ANGLE
OF
BANK
0
0
30°
45°
60°
KIAS KCAS
KIAS
KCAS
KIAS KCAS
KIAS
KCAS
UP
44
51
48
55
53
61 63 73
10°
35
48
38
52
42
58
50
69
30°
33
47
36 50
40
56
47
66
MOST
FORWARD
CENTER
OF GRAVITY
FLAP
SETTING
ANGLE
OF
BANK
0
0
30°
45° 60°
KIAS
KCAS
KIAS
KCAS
KIAS KCAS KIAS
KCAS
UP
44
52
48
56 53
62
63
74
10°
37
50
40
53
44
59
53
70
30°
33
47
36
50
40
56
47
66
NOTES:
1
.
Altitude loss
during
a
stall
recovery
may
be
as
much
as
230
feet.
2.
KIAS
values
are
approximate.
Figure
5-3.
Stall
Speeds
5-12
Dec
2/96
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