Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 99

CESSNA
MODEL T210M
SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
PRESSURE ALTITUDE 18,000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-41°C
RPM MP
%
KTAS PPH
BHP
2500 30
- -
-
- -
-
-
-
-
28
80 191 105
26
75
185 99
24
70 179
91
22
63 171 84
2400 30
81 192
107
28
76 186
100
26
71 180 93
24
66 174
87
22 61 167 80
2300
30
79 189 103
28
74 184 97
26
69
178
91
24
64
171 84
22
58 163 77
2200 26
66 174 87
24
61 166
80
~
22
55 157 73
20
49 146 66
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°CABOVE
TEMPERATURE STANDARD TEMP
-21°c
-1oc
%
KTAS PPH
%
KTAS PPH
BHP
BHP
81 196 106 76 194 100
76 190 99 71 188 93
71 184 93 67 182 88
66 177 86 62
174
81
60
168
79
• 56
165 75
77
191 101 72 189 94
72 185
94
67
183
88
67 179 88 63 176 83
62 172 82
58
169
77
57 164 76 54
160
72
74 188 97 70 186 91
70 183 91 65
180 86
65 176 86 61
173 81
60 169
79
56
165 75
55 160 73 51
155
69
62 172 82 58 169
77
57 164 76 54
160
72
51 154
69
48
149 66
46
142
63 43 136 59
Figure 5-7. Cruise Performance (Sheet 9 of 12)
5-25