Cessna TR182 1979 - Cruise Performance

CESSNA
MODELTR182
SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
PRESSURE ALTITUDE 2000 FEET
CONDITIONS:
3100 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
NOTE
For best fuel economy, operate at the
leanest mixture that results in smooth
engine operation or at peak EGT.
20°C BELOW STANDARD
20°C ABOVE
STANDARD TEMP TEMPERATURE
STANDARD TEMP
-9
0
e 11
0
e
31°C
RPM
MP
%
KTAS
GPH
%
KTAS GPH
%
KTAS
GPH
BHP
BHP
BHP
2400
25 - - -
- - -
- - -
78 150
14.8
74 149
14.0
23 74
143 14.0
70
143
13.3
66 143
12.6
21
65
136
12.4
62 136
11.8
59
135
11.3
19 57 128 10.9
54
128
10.5
51 127 10.0
2300
25 78
147 14.9 74 147
14.1
71 147
13.4
23 70
141
13.3 67
140
12.7
63 140
12.1
21
62
133
11.8
59 133
11.3
56
132 10.8
19 54
125
10.4
51 125
10.0 49
123
9.6
2200
25 75
144 14.2 71 144
13.5
67 144
12.8
23 67
138 12.1
64
131
12.1
60 131
11.5
21 59
130 11.3
56
130
10.8
53 129
10.3
19
51
122
9.9
49
121
9.5 46
120
9.1
2100
25
n
141
13.5 68
141
12.9 64
141 12.2
23
64
134
12.1 60
134
11.5
57 133
11.0
21
56
127
10.7 53
127
10.3
50 125
9.8
19
48 118 9.5 46 117
9.1 43
115
8.7
17
41 108 8.2
39
105
1.8
37 102 7.5
Figure 5-7. Cruise Performance (Sheet 1 of 10)
1 October 1978 5-17