Cessna T206H - Cruise Performance Pressure Altitude 24,000 Feet

ISSUED:
DATE: 8/4/2017
AFMS No.: 55186-5
Rev.: 1
Page: 30 of 36
Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna T206H
CRUISE PERFORMANCE
PRESSURE ALTITUDE 24,000 FEET
CONDITIONS:
3789 Pounds
Recommended Lean Mixture Cowl Flaps CLOSED
RPM MP
(in. Hg.)
20°C BELOW
STANDARD TEMP
-53°C
STANDARD
TEMPERATURE
-33°C
20°C ABOVE
STANDARD TEMP
-13°C
% MCP KTAS GPH % MCP KTAS GPH % MCP KTAS GPH
2400
30 ----- ----- ----- ----- ----- ----- ----- ----- -----
28 72
159
18.4 68
157
17.3 63
150
16.2
26 67
153
17.2 64
150
16.2 60
144
15.2
24 62
145
15.9 58
139
15.0 55
129
14.0
22 58
138
14.9 55
131
14.1 -----
-----
-----
20 54
129
13.7 -----
-----
----- -----
-----
-----
2300
30 ----- ----- ----- ----- ----- ----- ----- ----- -----
28 68
154
17.5 64
150
16.4 60
144
15.4
26 64
148
16.3 60
143
15.4 56
133
14.4
24 59
140
15.0 55
131
14.1 -----
-----
-----
22 55
132
14.0 52
121
13.2 -----
-----
-----
2200
30 ----- ----- ----- ----- ----- ----- ----- ----- -----
28 65
150
16.6 61
145
15.6 57
136
14.6
26 60
142
15.4 57
136
14.5 -----
-----
-----
24 55
132
14.1 52
121
13.3 -----
-----
-----
22 51
120
13.1 -----
-----
----- -----
-----
-----
2100
30 ----- ----- ----- ----- ----- ----- ----- ----- -----
28 64
148
16.2 60
143
15.3 56
133
14.4
26 59
140
15.1 56
134
14.3 -----
-----
------
24 54
129
13.8 -----
-----
----- -----
-----
-----
2000
30 ----- ----- ----- ----- ----- ----- ----- ----- -----
28 62
145
15.9 59
141
15.0 55
129
14.1
26 58
138
14.9 55
131
14.0 -----
-----
-----
24 53
127
13.5 -----
-----
----- -----
-----
-----
NOTE
 For best economy, operate at peak T.I.T.
 Some power settings may not be obtainable, but are listed to aid interpolation.
 Power settings not approved for cruising are indicated by dashes.
Figure 5-9 (Sheet 12)