Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 102

SECTION 5
PERFORMANCE
CESSNA
MODEL T210M
CRUISE PERFORMANCE
PRESSURE ALTITUDE 24,000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-53°C
RPM MP
%
KTAS PPH
BHP
2500 28
79 200
104
26 74 194 97
24
68
186 90
22
62 177 82
2400 28
75
195 99
26
70
188 92
24
65 181 85
22
60
173 79
2300
26
69 187 91
24
65
181 85
22
60 173
79
20 55 164 74
2200 22
56
165 74
20
50 154 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
-33°C -13°C
%
KTAS
PPH
%
KTAS
PPH
BHP BHP
74
198 98 70
196
92
70
192 91
65
188
86
64
183 85 60
179 80
59
174 78
55
169
74
71
193 93
66
190 87
66
186 87
62
182
82
61
178 81 57
173
76
57
170 75 53
164 71
65
185 86 61
181
81
61
178 81
57
173
76
57
170 75
53
164 71
52
160 70 49
154
66
52
161 70 49
155
66
47
148 64
44
141
61
Figure 5-7. Cruise Performance (Sheet 12 of 12)
5-28