CESSNA
MODEL 172N
SECTION 5
PERFORMANCE
STALL SPEEDS
CONDITIONS:
Power Off
NOTES:
1.
Maximum altitude loss during a stall recovery may be as much as 180 feet.
2.
Kl AS values are approximate.
MOST REARWARD CENTER OF GRAVITY
ANGLE OF BANK
WEIGHT
FLAP
oo
30
°
45
°
LBS
DEFLECTION
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
UP
39
50
42
54
47
59
2300
100
38
47
40
51
45
56
400
31
44
33
47
37
52
MOST FORWARD CENTER OF GRAVITY
ANGLE OF BANK
WEIGHT
FLAP
oo
30
°
45
°
LBS
DEFLECTION
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
UP
44
53
47
57
52
63
2300
100
44
51
47
55
52
61
40
°
33
47
35
51
39
56
Figure 5-3. Stall Speeds
1 July
1979
60
°
KIAS
KCAS
56
71
54
66
45
62
50
0
KIAS
KCAS
62
75
62
72
47
66
5-11