Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 95

CESSNA
MODEL T210M
SECTION 5
PERFORMANCE
\
CRUISE PERFORMANCE
PRESSURE ALTITUDE 10,000 FEET
CONDITIONS:
3800 Pounds
,Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-25°C
RPM MP
%
KTAS PPH
BHP
2500
30
- - -
- -
-
- - -
28
80
176
105
26 75
172 98
24 69 166
90
22 62 158
81
2400 30
81 ·
177
107
28
76 173 99
26 70 167
92
24
64 160
84
22
58 153 77
2300 30 78
175 103
28 -
73. 170 . · 96
26
67 164 88
24 61 157
81
22
55
149 73
2200 30
74 171 97
28
69 166
90
26
63 160
84
24 58
153
77
22
52 144 70
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
-5°C
15°c
%
KTAS
PPH
%
KTAS PPH
BHP BHP
81
182 107 76 181
100
76
177
99
71
175
93
71
171 92 66
170
87
65 164
85 61
162
80
58
156 77 55 153
73
77
178
101
72
176
94
71
172 94 67 171
88
66 166
87
62 164
82
60
159 80 57
157
75
55
151 73 51
148
69
74
175 97 69 173
91
69
169 90 65 168
85
64
163 84 60
161
79
58 156
77
54
153
73
52 147 70 49 143
66
70
170 92 66 169
86
65
165 85 61 163 81
60
158 79
56 156
75
54 151 73
51 148
69
49
142 66 46 138
63
..
Figure 5-7. Cruise Performance (Sheet 5 of 12)
5-21