Stall Speeds - Cessna 172 P Pilot Operating Handbook

SECTION: | 1 | 2 | 3 | 4
S T A LL S P E E DS
CONDITIONS:
Power Off
NOTES:
1. Altitude loss during a stall
recovery may be as much as 230
feet.
2. KIAS values are appoximate.
MOST REARWARD CENTER OF GRAVITY
WEIGHT FLAP
LBS DEFLECTION
UP
2400 10°
30°
MOST FORWARD CENTER OF GRAVITY
WEIGHT FLAP
LBS DEFLECTION
UP
2400 10°
30°
| 5 | 6 | SUPP |
ANGLE OF BANK
0° 30°
KIAS KCAS KIAS KCAS
44 51 47 55
35 48 38 52
33 46 35 49
ANGLE OF BANK
0° 30°
KIAS KCAS KIAS KCAS
44 52 47 56
37 49 40 53
33 46 35 49
45° 60°
KIAS KCAS KIAS KCAS
52 61 62 72
42 57 49 68
39 55 47 65
45° 60°
KIAS KCAS KIAS KCAS
52 62 62 74
44 58 52 69
39 55 47 65
Figure 5-3 Stall Speeds
PERFORMANCE
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