Cessna 172P Pilot's Operating Handbook And Flight Manual page 206

1
FLOATPLANE
MODEL
17AP
PILOT'S OPERATING HANDBOOK
SIIPPLEMENT
STALL SPEEDS
CONDITIONS:
Power
Off
NOTES:
L
Altitude
loss
during
a
stall
recovery may be
as
much
as
2ü)
feet.
2.
KIAS valucs
arc approximate
MOST REARWARD CENTER OF GRAVITY
MOST FORWARD CENTER OF GRAVITY
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF
BANK
go
300
45() 6oo
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
2220
UP
100
300
38
35
36
48
46
44
41
38
39
52
49
47
46
42
44
57
55
52
55
50
53
68
65
62
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF
BANK
Oo
300
450 600
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
2220
UP
100
300
41
37
36
50
47
44
44
40
39
54
51
47
49
45
44
59
56
52
58
5,4
53
71
66
62
22
Figure
5.
Stall
Speeds
30
May
1980