Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 97

CESSNA
MODEL T210M
SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
PRESSURE ALTITUDE 14,000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-33°C
RPM
MP·
%
KTAS PPH
BHP
2500 30
-
-
;'-
-
-
- -
- -
28
80
184 105
26
75 179
99
24
70 172 91
22
63 164
83
2400 30
82 185 107
28
76 180 100
26
71 174
93
24
65
167
86
22
60 160
79
2300
30
79
182 104
28
74
177 97
26
68 171
90
24
63 164
83
22
57
156 75
2200 28
70
173 92
26
65 167
85
24
59
160 78
22
53 151
71
20
47
140 64
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
-13°C
1°c
%
KTAS PPH
%
KTAS
PPH
BHP BHP
81 189 107 76 187 100
76 183
99
71
182 93
71 178 93
67
176 88
66 171 86
62
169 81
59
163 78
56 160 74
77 184 101
72
183 95
.1~2-
179 94
67
177 89
67 173
88
63 170 83
61 166
81
58 163 77
56 158 75
53
154 71
74
182 98
70
180
92
70 176 92
66
174 86
61r-·
-no·· ···i:nr
61
167 80
59 162 78
55
159
74
53 153
72
50 150 68
66 172 87
62.
169
82
61 165 81
57
162 76
56 157
74 52 154 70
50 148 68
47
143 64
45 136 61
42 131 58
Figure 5-7. Cruise Performance (Sheet 7 of 12)
5-23