Cessna 172P - 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