Cessna R182 - Page 77

CESSNA
MODEL
R182
SECTION
5
PEF,FORMANCE
STALL
SPEEDS
'-
CONDITIONS:
Power
Off
NOTES:
1.
Maximum altitude
loss
during
a stall recovery
may be
as much
as
240
feet.
2. KIAS
values
are
approximate;
MOST REARWARD
CENTER
OF GRAVITY
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE
OF
BANK
Oo
300
450
600
KIAS
KCAS
KIAS KCAS
KIAS KCAS
KIAS
KCAS
3100
UP
200
400
zlt)
38
35
54
51
50
43
41
38
58
55
g
/18
I
43
tr
61
59
57
55
52
76
72
71
MOST FORWARD
CENTER
OF GRAVITY
WEIGHT
LBS
FLAP
DEFLECTION
ANGLE OF
BANK
0o
300
450
600
KIAS
KCAS KIAS
KCAS
KIAS KCAS KIAS
KCAS
3100
UP
2e
4@
42
40
37
55
52
52
45
41
4
59
56
56
50
6
45
65
62
62
59
55
il
78
74
74
Figure
5-3. Stall Speeds