Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 92

SECTION 5
PERFORMANCE
CESSNA
MODEL T210M
CRUISE PERFORMANCE
PRESSURE ALTITUDE 4000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c
BELOW
STANDARD TEMP
-13°C
RPM
MP
%
KTAS PPH
BHP
2500
30
- - -
-
- - - - -
28 79 166
103
26
72
160
95
24 65 154
86
22 58
146
77
2400
30
80
167
105
28 74 162
97
26 68 156
89
24
61 150
81
22 55 142
73
2300
30
77
164
100
28 71 159
93
26 65
154
85
24
59
147
78
22 52 139
70
2200
30 73 161
95
28 67 156
88
26
61 149
80
24 55
142
73
22 49 135
67
NOTE
For best fuel economy at 70% power or less, op-
,erate at 6 PPH leaner than shown in th is chart
or at peak EGT if an EGT indicator is installed.
STANDARD 20°c ABOVE
TEMPERATURE STANDARD TEMP
1°c 21°c
%
KTAS PPH
%
KTAS PPH
BHP
BHP
81
171 106
76
171
100
74 166 97
70 165 91
68
160 90
64
159
84
62 153 81
58
152
77
55
145 73
51
142 69
76 167 99
71
167 93
70
162 92
66
161
86
64 156 84
60
154 79
58
149
77
54
147
73
52 141 70
49
138 66
72
164 95
68
163
89
67 159 88
63
157
83
61
153 81
58
151 76
55
146 74
52
143
70
49 137
67
46
134
63
68
161 90
64
159 84
63
155 83
59
153 78
57
148
76 54
146
72
52
141 70
49
138
66
46 132 63 44 129 60
Figure 5-7. Cruise Performance (Sheet 2 of 12)
5-18