Cessna 17273274 Pilot Operating Handbook page 86

SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
CONDITIONS:
2300 Pounds
Recommended Lean Mixture
20
PRESSURE
STANDARD TEMP
RPM
ALTITUDE
%
FT
BHP
2000 2500 - - -
72
2400
64
2300
2200 56
50
2100
-
4000 2550
- -
76
2500
68
2400
60
2300
2200 54
2100 48
6000 2600
- - -
2500 72
64
2400
2300 57
2200 51
2100 46
-
8000 2650
- -
76
2600
68
2500
61
2400
2300 55
2200 49
2650 76
10,000
2600 72
2500 65
2400 58
52
2300
2200 47
68
12,000 2600
62
25 gg
24 56
2300 50
2200 46
Figure 5 - 7. Cruise Performance
5-16
C BELOW
°
STANDARD
TEMPERATURE
%
GPH
KTAS
BHP
-
-
- - - - 75
111
8.0 67
106
7.1 60
101
6.3 53
95
5.8 47
-
75
- - - - -
116
8.5 71
111
7.6 64
105
6.8 57
100
6.1 51
94 46
5.6
-
75
- - -
- -
116
8.1 67
110
7.2 60
105
6.5 54
99
5.9 49
93
5.5 44
- - - -
.
75
-
120
8.6 71
115
7.7 64
110
6.9 58
104
6.2 52
98
5.7 47
122
8.5
71
120
8.1 68
114
61
7.3
109
6.5 55
103
6.0 50
97
5.6 45
119
7.7 64
114
6.9 58
108
6.3 53
102
48
5.8
96 44
5.5
MODEL 172N
20 C ABOVE
°
STANDARD TEMP
%
GPH
KTAS
KTAS
BHP
116 71 115
8.4
111 63 110
7.5
105 6.7 105
56
100 6.1 50
94 5.6 45
118 8.4 118
71
115 8.0 67 115
110 7.1 60 109
104
105 6.4 54
48
99 5.9
93 5.5
44
120 8.4 71 120
114
115 7.6 64
109
109 6.8 57
103
104 6.2 52
47
98 5.7
92 42
5.4
122
122 8.4 71
119
120 8.0 67
113
114 7.2 60
108
109 6.5 55
102
103 6.0 50
45
97 5.5
67 121
122 8.0
118
119 7.6 64
112
114 6.8 58
107
108 6.2 52
101
102 5.8 48
44
96 5.4
117
61
118 7.2
6.5 55 111
113
106
107 6.0 51
100
101 5.6 46
43
95 5.4
CESSNA
GPH
7.9
7.1
6.3
5.8
99
5.4
93
7.9
7.5
6.7
6.1
98 5.7
5.3
92
7.9
7.1
6.4
5.9
5.5
97
5.2
91
7.9
7.5
6.8
6.2
5.8
5.4
96
7.5
7.1
6.5
6.0
5.6
5.3
95
6.8
6.2
5.8
5.5
5.3
94
1 July 1979