Cessna 172R Pilot Operating Handbook page 126

STALL SPEEDS AT 2450 POUNDS
Conditions:
Power Off
MOST REARWARD CENTER OF GRAVITY
MOST FORWARD CENTER OF GRAVITY
NOTES:
Altitude loss during a stall recovery may be as much as 230 feet.
KIAS values are approximate.
Figure 5-3. Stall Speeds
FLAP
SETTING
ANGLE OF BANK
0° 30° 45°
60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP
100
30°
44
35
33
I
51
48
47
48
38
36
55
52
50
53
42
I
40
61
58
I
56
63
50
47
73
69
I
66
FLAP
SETTING
ANGLE OF BANK
0°
3C,I°
I
45°
60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP
100
30°
44
37
33
52
50
47
48
40
36
56
53
50
53
44
40
62
59
56
63
53
47
74
70
66
SECTION 5
CESSNA
PERFORMANCE
MODEL 172R
5-12
Dec 2/96
1.