Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 94

SECTION 5
PERFORMANCE
CESSNA
MODEL T210M
CRUISE PERFORMANCE
PRESSURE ALTITUDE 8000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-21°c
RPM MP
%
KTAS
PPH
BHP
2500 30
-
- - - - - - -
-
28
80 173 105
26
74 168 97
24
68 162 89
22
60 154
80
2400
30
81 174 106
28
75 169 99
26
69 164 91
24
63 157
83
22
57 150
76
2300 30
78 171 102
28
72
167 95
26
67 161 87
24
60 154 80
22
54 146
72
2200
30
73 167 96
28
68 162 89
26
63
156
82
24
57
149
75
22
51
141
69
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
-1°C
19°c
%
KTAS
PPH
%
KTAS
PPH
BHP
-·
BHP
81
178 107 76 178 100
75,
173 99~ 71
172
93
70 168 91 65
166
86
64 161 84 60
159
79
57
152 76 53
150
72
76
174 100
72
173 94
71
169
93
67 167 87
,... 65
162 86 61
161 81
60
156
79
56
153 74
54
t48
72
51
145
68
73
171
96 69
170 90
68
166 90
64 164 84
63
160
83
59 158 78
57 152 76
54
150
72
51
144 69 48
140
65
69
167 91
65
165 86
64 161 85 60
159 80
59
155 78 55
152 74
54
147
72
50
144
68
48 138 65
45 135 62
Figure 5-7. Cruise Performance (Sheet 4 of 12)
5-20