Cessna T182 1982 Pilot Operating Handbook page 92

SECTION 5 CESSNA
PERFORMANCE MODELT182
CRUISE PERFORMANCE
PRESSURE ALTITUDE 12.000 FEET
CONDITIONS:
3100 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°C BELOW
STANDARD 20°C ABOVE
STANDARD TEMP TEMPERATURE STANDARD TEMP
-29°C
-9°C
11°C
RPM MP
%
KTAS GPH
%
KTAS
GPH
%
KTAS GPH
BHP BHP
BHP
2400 25 - -
-
- -
-
-
- -
79 151
15.0 75
150 14.3
23 76
145 14.5
73
145 13.8
69
144 13.1
21 69
139 13.2
66 138
12.5 62
137 11.9
19
62 132 11.9
59
131
11.3 56
130 10.8
2300
25
80
148 15.2
76 148
14.5
72
147 13.7
23 73
143 13.9
70 142
13.2 66
141 12.6
21 66
136 12.6
63 136
12.0 60
134 11.5
19 60 129
11.4
57 128
10.9 54
126 10.4
2200 25
77
146 14.6
73 146
13.9 69
145 13.2
23
70 140 13.3
67
139
12.7 63 138
12.1
21 64
133 12.1
61
133
11.6 57
131 11.0
19 57
126 11.0
54
125 10.5
51 123
10.0
2100 25
74 143 14.0
70
143
13.3 66
142 12.6
23 67
137 12.8
64
136 12.2
61 135
11.6
21
61
131 11.6
58
130
11.1 55
128 10.6
19 54
123 10.5
52
122 10.1
49
119
9.6
17 48 115 9.4
46 112
9.0 43
108 8.6
\
Figure 5-8. Cruise Performance (Sheet 6 of 10)
NOTE
For best fuel economy, operate at the
leanest mixture that results in smooth
engine operation or at peak EGT.
(
,
\
/
5-24 21 August 1981