Cessna 208B - Page 181

SECTION 5
PERFORMANCE
CESSNA
MODEL
2088 (675 SHP)
STALL SPEEDS
Conditions:
Power Lever
- ldle
Fuel Condition Lever - High ldle
1 Weight - 8750 Lbs
NOTE
1. Altitude loss during a stall recovery may be as much as 300
feet from a wings-level stall and even greater from a turning
stall.
2. KlAS values are approximate.
MOST REARWARD CENTER OF GRAVITY
8750 Pounds:
I I FLAP 1 ANGLE OF BANK I
.
1
Figure 5-6. Stall Speeds
MOST FORWARD CENTER OF GRAVITY
8750 Pounds:
I FLAP ANGLE OF BANK
1 5-18 U.S. Revision 23
SETTING
UP
10'
20'
30'
1
SETTING
UP
10'
20'
30'
0'
KlAS
63
58
53
48
KCAS
78
69
63
60
30"
0'
KlAS
68
62
57
52
KlAS
63
60
54
50
KCAS
8-4
74
68
64
45"
KCAS
78
70
64
61
30"
KlAS
75
69
63
57
60"
KlAS
68
64
58
54
KCAS
93
82
75
71
KlAS
89
82
75
68
45"
KCAS
84
75
69
66
KCAS
110
98
89
85
KlAS
75
71
64
59
60"
KCAS
93
83
76
73
KlAS
89
85
76
71
KCAS
110
99
91
86