CESSNA
MODEL 172R (180 HP)
SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
CONDITIONS:
2550 Pounds
Recommended Lean Mixture At All Altitudes (Refer to Section 4,
Cruise)
PRES!
2o·c BELOW
STANDARD
20
°
CABOVE
STANDARD TEMP TEMPERATURE
STANDARD TEMP
ALT
RPM
%
KTAS
GPH
%
KTAS
GPH
%
KTAS
GPH
BHP
BHP
BHP
2000 2550
83
117
11.1
77
118
10.5
72
117
9.9
2500
78
115
10.6
73
115
9.9
68 115
9.4
2400
69
111
9,6
64
110
9.0 60
109
8.5
2300
61
105
8.6
57 104
8.1
53
102 7.7
2200
53
99
7.7
50
97
7.3
47
95
6.9
2100
47
92
6.9
44
90
6.6
42
89 6.3
4000
2600
83
120
11.1
77
120
10.4
72 119
9.8
2550 79
118
10.6
73
117
9.9
68
117
9.4
2500
74
115 10.1
69
115
9.5
64
114
8.9
2400
65
110
9.1
61
109
8.5 57
107
8.1
2300
58
104
8.2 54
102
7.7 51
10�
7.3
2200 51
98
7.4
48
96
7.0
45
94
6.7
2100
45
91
6.6
42
89
6.4
40
87
6.1
6000
2650
83
122
11.1
77
122
10.4
72
121
9.8
2600 78 120
10.6
73
119
9.9
68
118
9.4
2500
70
115
9.6
65
114
9.0
60
112
8.5
2400
62
109
8.6
57
108
8.2
54
106
7.7
2300
54
103
7.8
51
101
7.4
48
99
7.0
2200
48
96
7.1
45
94
6.7
43 92
6.4
NOTE:
1. Cruise speeds are shown for an airplane equipped with speed fairings.
Without speed fairings, decrease speeds shown by 2 knots.
""
Figure 5-8. Cruise Performance (Sheet 1 of 2)
Oct 4/01
5-19
Summary of Contents for 172R180HP
Page 4: ...I I I _ I l...
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Page 15: ...t GENERAL...
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Page 187: ...AIRPLANE SYSTEMS DESCRIPTIONS...
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Page 239: ...co HANDLING _ SERVICE MAINTtNANCE...
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