Cessna TR182 1979 - Stall Speeds

CESSNA
MODEL TR182
SECTION 5
PERFORMANCE
STALL SPEEDS
CONDITIONS:
Power Off
NOTES:
1. Maximum altitude loss during a stall recovery may be as much as 300 feet.
2. KIAS values are approximate.
MOST REARWARD CENTER OF GRAVITY
ANGLE OF BANK
WEIGHT
FLAP
0
0
30° 45°
60°
LBS DEFLECTION
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP
41
54
44
58 49
64 58
76
3100
20° 39 51
42
55 46
61 55
72
40° 40 50
43 54 48
59
57
71
MOST FORWARD CENTER OF GRAVITY
ANGLEOF BANK
WEIGHT
FLAP
0°
30° 45° 60°
LBS
DEFLECTION
KIAS
KCAS KIAS KCAS KIAS
KCAS KIAS KCAS
UP 43
55
46
59
51
65 61
78
3100
20°
41
52
44 56
49
62 58
74
40°
43
52 46
56 51
62 61
74
Figure 5-3. Stall Speeds
1 October 1978
5-11