Cessna T182 1982 Pilot Operating Handbook page 90

SECTION 5
CESSNA
PERFORMANCE
MODEL T182
CRUISE PERFORMANCE
PRESSURE ALTITUDE 8000 FEET
CONDITIONS:
NOTE
3100 Pounds
Recommended Lean Mixture For best fuel economy, operate at the
Cowl Flaps Closed leanest mixture that results in smooth
engine operation or at peak EGT.
20°C BELOW STANDARD 20°C ABOVE
STANDARD TEMP
TEMPERATURE STANDARD TEMP
-21°C -1°C
19°C
RPM MP
%
KTAS GPH
%
KTAS GPH
%
KTAS GPH
BHP BHP BHP
2400 25
.
--
- -- - - -
79 146 15.1 75 145
14.3
23 76 140 14.4 72
140 13.7
69 139 13.0
21 68 134 13.0 65
133 12.4
62 132 11.8
19
61 126 11.6 58
126 11.1 55 124
10.6
2300 25
80
143 15.2 76
143 14.5 72
143 13.7
23 73 137 13.8 69
137 13.1
66 136 12.5
21 65 131 12.4 62
130
11.9
59
129 11.3
19
58
123 11.1 55 123
10.6
52 121 10.1
2200 25 77
141 14.6 73
140
13.9 69 140 13.1
23 70 135 13.2 66
134 12.6
63 133 12.0
21 62 128 11.9 59
127 11.3
56
126
10.8
19 55
121
10.6 53
120 10.2 50 118
9.7
2100 25
73
138 13.9 70
138 13.2
66 137 12.6
23
66
132 12.6 63
131 12.0
60 130 11.4
21
59
125 11.3 56
124 10.9 54
123 10.4
19
52
117
10.2
50 116 9.7 47 114 9.3
17 46 108 9.0 43
106 8.6 41
102 8.3
Figure 5-8. Cruise Performance (Sheet 4 of 10)
(
I
5-22
21 August 1981