Cessna T182 1982 Pilot Operating Handbook page 77

CESSNA
MODEL T182
P
SECTION 5
ERFORMANCE
AIRSPEED CALIBRATION
NORMAL STATIC SOURCE
CONDITIONS:
Power required for level flight or maximum power descent.
FLAPS UP
KIAS
KCAS
FLAPS 20
0
KIAS
KCAS
FLAPS FULL
KIAS
I
KCAS
50
61
40
54
40
52
60
65
50
58
50
57
70
72
60
63
60
63
80
80
70
71
70
71
90
89
80
80
80
80
100
99
90
89
90
90
110
109
95
94
95
95
120 130 140 150
118
128
138
147
-
­ -
-
­
- - -
­
- - -
- ­
-
- -­ -
­ -
-
­
-
-
- - -
­ -
- ­
-
-
­ -
-
- ­
-
-
­
-
-
­
-
­ -
160
157
- - -
- - -
- -
-
- - -
170
167
- -­
-
- -
- -
­
- ­ -
I
I
Figure 5-1. Airspeed Calibration (Sheet 1 of 2)
21 August 1981
Revision 1 - 4 December 1981
5-9