Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 101

r--
CESSNA
MODEL T210M
SECTION 5
PERFORMANCE
CRUISE PERFORMANCE
PRESSURE ALTITUDE 22,000 FEET
CONDITIONS:
3800 Pounds
Recommended Lean Mixture
Cowl Flaps Closed
20°c BELOW
STANDARD TEMP
-49°C
RPM MP
%
KTAS
PPH
BHP
2500
30 - - -
- - -
- -
-
28 80
197 104
26 75
191 98
24
69
184
91
22
63
175 83
2400
30 80
197 105
28 76
192
99
26 71
186
93
24
66
179
86
22 61
172
80
2300
26 69
184 91
24
65
178 85
22 59
170
79
20
54
161 73
2200 24
61
173 81
22
56
163 74
20
50
151
67
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
-29°c
_9oc
%
KTAS PPH
%
KTAS PPH
BHP BHP
80
202 104 75 199
98
75 196
98
70 193
92
70 190
92
66
186 87
65 182
86
61 178
81
59 173
79 56
168 74
75
,1.96
99
71
194
93
· - r,
191
93 67 188
88
67 184
87
62
181 82
62 177
82
58
172
77
57
168 76 54 163
72
65 182
86
61
178 81
61
175.
80
57 171
76
56 166 75 53 161 71
51 157
69
48
151 65
58 170 77 54 165
73
52 159
70
49
154 67
47 147
64
44
140
61
Figure 5-7. Cruise Performance (Sheet 11 of 12)
5-27