Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 96

SECTION 5
PERFORMANCE
CESSNA
MODEL T210M
CRUISE PERFORMANCE
PRESSURE ALTITUDE 12,000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-29°C
RPM MP
%
KTAS PPH
BHP
2500
30
-
-
-
- - - - - -
28 80 180
105
26
75
175
98
24
69
169
90
22
62 161 82
2400 30
81 181 107
28 76 176
99
26
70
170
92
24
65 164 85
22 59 156
78
2300
30 79 179 103
28
73 174- 96
26 68 167
-~~)
24 62 161 82
22
56 152
74
2200
28
69 169 91
26
64
163
84
24 58 156 77
22
52 147
70
20
46 137 63
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.
•,
20°CABOVE STANDARD '
·,
TEMPERATURE /
STANDARD TEMP
_9oc .
110c
%
KTAS PPH
%
KTAS
PPH
BHP BHP
81 185 107 76 184 100
76 18. 0 99 71 178 93
71 174 93 66 173 87
65
168 · 85-
61
166 81
59 159 78 55 156 73
77 181 101
72
179 94
71 175
94 67 174 88
66 169
87 62 167
82
61 162 80 57 160 76
55
155
74 52 151 70
74 178
97 70 177 91
69
173 91 65 171 85
64
166
84 60 164 79
58 159
77
55
156 73
53 150
71 49
146
67
65 168 86
61 166 81
60 162 80
57 159
75
55 154
73 52 151 70
49 144 67 46 140 63
44
133
60 41 129 57
Figure 5-7. Cruise Performance (Sheet 6 of 12)
5-22