Cessna 206H - Page 107

SOLOY TURBINE PAC SECTION 5
POHS CESSNA T206H/206H PERFORMANCE
5-7
F.A.A. Approved May 23, 2003
MOST FORWARD CENTER OF GRAVITY
WEIGHT
LBS.
FLAP
DEFLECTIO
N
ANGLE OF BANK
0
30
45
60
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
3600
0
49
58
54
62
64
69
79
82
3600
20
42
53
48
57
56
63
71
75
3600
40
40
52
52
56
60
62
74
74
Figure 5-3. Stall Speeds (Sheet 2 of 2)
UNCONTROLLED
COPY