Cessna 172P - Page 83

CESSNA
MODEL 172P
STALL
SPEEDS
CONDITIONS:
Power
Off
NOTES:
1. Altitude loss during a stall recovery
may
be
as
much
as
230 feet.
2,
KIAS
values are approximate.
MOST
REARWARD
CENTER
OF
GRAVITY
MOST FORWARD
CENTER
OF
GRAVITY
SECTION
õ
PEN,FORMANCE
I
\
è
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF BANK
Oo 300
450
6oo
KIAS KCAS
KIAS
KCAS
KIAS
KCAS KIAS
KCAS
2400
UP
100
300
44
35
33
51
48
46
47
38
35
55
52
49
52
42
39
61
57
55
62
49
47
72
68
65
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF BANK
Oo
300
450
60o
KIAS
KCAS
KIAS
KCAS
KIAS KCAS
KIAS
KCAS
2400
UP
100
300
44
37
33
52
49
46
47
40
35
56
53
49
52
44
39
62
58
55
62
52
47
74
69
65
30
May
1980
Figure
5-3.
Stall Speeds
5- 11