Cessna T182 1982 Pilot Operating Handbook page 94

SECTION 5
CESSNA
PERFORMANCE
MODEL T182
CRUISE PERFORMANCE
PRESSURE ALTITUDE 16.000 FEET
CONDITIONS:
3100 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°C BELOW
STANDARD TEMP
-37°C
STANDARD
TEMPERATURE
-17°C
20°C ABOVE
STANDARD TEMP
3°C
RPM MP
%
BHP
KTAS
GPH
%
BHP
KTAS GPH
%
BHP
KTAS GPH
2400 25
23
21
19
-
­ -
76
70
63
-
­
-
150
144
137
- -
.
14.4
13.2
12.0
78
72
66
60
155
150
143
136
14.8
13.7
12.6
11.5
74
68
63
57
155
149
142
134
14.1
13.0
12.0
10.9
2300
25
23
21
19
79
73
67
61
153
148
141
135
15.1
13.9
12.7
11.6
75
70
64
58
153
147
141
133
14.3
13.2
12.1
11.1
72
66
60
55
152
146
139
131
13.6
12.6
11.5
10.6
2200 25
23
21
19
76
70
64
58
150
145
139
132
14.5
13.4
12.3
11.2
73
67
61
56
150
144
138
130
13.8
12.7
11.7
10.7
69
64
58
53
149
143
136
128
13.1
12.1
11.1
10.2
2100
25
23
21
19
17
73
68
62
56
50
148
142
136
129
120
14.0
12.9
11.8
10.8
9.8
70
64
59
53
48
147
141
135
127
118
13.3
12.2
11.3
10,3
9.4
66
61
56
51
45
146
140
133
124
113
12.6
11.6
10.7
9.9
9.0
NOTE
For best fuel economy, operate at the
leanest mixture that results in smooth
engine operation or at peak EGT.
I
I
I
Figure 5-8. Cruise Performance (Sheet 8 of 10)
5-26
21 August 1981