Cessna T182 1982 Pilot Operating Handbook page 80

SECTION 5
CESSNA
PERFORMANCE MODEL T182
STALL SPEEDS
(
CONDITIONS:
Power Off
NOTES:
1. Altitude loss during a stall recovery may be as much as 300 feet.
2. KIAS values are approximate.
MOST REARWARD CENTER OF GRAVITY
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE OF BANK
0°
30°
45° 60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
3100
UP
20°
FULL
44
,
37
33;
54
50
49
47
40
35
58
54
53
52
44
39
64
60
58
62
52
47
76
71
69
I
I
MOST FORWARD CENTER OF GRAVITY
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE OF BANK
0° 30°
45°
60°
KIAS
KCAS
KIAS KCAS KIAS
KCAS KIAS KCAS
3100
UP
20°
FULL
48
43
40
56
53
52
52
46
43
60
57
56
57
51
48
67
63
62
68
61
57
79
75
74
Figure 5-3. Stall Speeds
21 August 1981
Revision 1 - 4'December 1981
5-12
I