Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 93

CESSNA
MODEL T210M
SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
PRESSURE ALTITUDE 6000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-17°C
RPM MP
%
KTAS PPH
BHP
2500
30
-
-
-
-
-
-
-
- -
28 79
169
104
26
73
164
96
24 67
158
88
22 59
150
79
2400
30
81
170
106
28
75
166
98
26 69
160
90
24 62
153
82
22 56
146
75
2300
30
77
168
101
28
72
163
94
26 66
157
87
24 60
150
79
22 53
142
72
2200 30 73
164
96
28 68
159
89
26 62
153
82
24 56
146
75
22
50
138
68
NOTE
For best fuel economy at 70% power or less, op-
erate at 6 PPH leaner than shown in this chart
or at peak EGT if an EGT indicator is installed.
STANDARD
20°c ABOVE
TEMPERATURE STANDARD TEMP
3°c
23°c
%
KTAS PPH
%
KTAS PPH
BHP BHP
81
175
107
76 175
100
75
170
98
70
169
92
69
164
91
65
163
85
63 157
83
59
155
78
56
149
75
53
146
71
76
171
100
72
170
94
71
166
93
66 164
87
65
159
85
61 158
80
59
152
78 55 150
74
53
144
71
50 142
67
73
168
96 69
166
90
68
163
89 64
161
84
62 156 82
58
154
77
56
149
75
53
147
71
50
141
68 47 138
64
69
164
90
65
162
85
64 158
84 60 156
79
58
152
77
55
149
73
53
144
71
50
141
67
47
135
64
44
132
61
Figure 5-7. Cruise Performance (Sheet 3 of 12)
5-19