Cessna T182 1982 Pilot Operating Handbook page 96

SECTION 5
CESSNA
PERFORMANCE
MODEL T182
CRUISE PERFORMANCE
PRESSURE ALTITUDE 20,000 FEET
CONDITIONS:
3100 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°C BELOW
STANDARD 20°C ABOVE
STANDARD TEMP TEMPERATURE STANDARD TEMP
-45°C
-25°C - 5°C
RPM
MP
%
KTAS
GPH
%
KTAS
GPH
%
KTAS GPH
BHP
BHP
BHP
2400 25
-
-­
- -­ - -­
76 159
14.5
72 158
13.7
23 74
154
14.1 71 153 13.5 67 152
12.8
21
69 148
13.1 65 147 12.4
62
145
11.8
19
63 142
12.0 60 140 11.5 57 137
10.9
2300 25 77 157
14.7 74 156 14.0
70
155 13.3
23 72 152
13.7 69 151 13.0
65
149
12.4
21 67 146 12.7 63
145 12.1
60
142 11.5
19 61 139 11.7 58
137 11.1
55
134 10.6
2200
25 75
154
14.2 71 154
13.5
68 152
12.8
23
70 149
13.2 66 148 12.6
63
146
12.0
21
64 143
12.2 61 142
11.7
58
139
11.1
19 59 136 11.3 56
134 10.8
53 131
10.3
2100
25
72 152
13.8 69
151
13.1
65 150
12.4
I
23 67 146 12.8
64
'45
12.2 61 143 11.6
21 62 140
118
59
1:19
11.3
56 136
10.8
19
57
134
10.9
54 131
10.5
51 127
10.0
17
52 126 10.1
49
122
9.6 47 116
9.2
Figure 5-8. Cruise Performance (Sheet 10 of 10)
NOTE
For best fuel economy, operate at the
leanest mixture that results in smooth
engine operation or at peak EGT.
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5-28 21 August 1981