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Cessna
Stationair
Performance
Improvements
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click on image to enlarge |
On Wheels
Climb Data*
Altitude
MSL |
Engine
RPM |
Manifold
Pressure |
%
Power |
KIAS |
KTAS |
ROC
FPM |
| SL |
2575 |
43 |
100 |
100 |
100 |
1,350 |
| 4,000 |
2575 |
40 |
100 |
100 |
104 |
1,250 |
| 8,000 |
2300 |
38 |
80 |
100 |
111 |
1,150 |
| 15,000 |
2300 |
37 |
80 |
100 |
125 |
1,050 |
aircraft
comparison chart
Cruise Data*
Altitude
MSL |
Engine
RPM |
Manifold
Pressure |
%
Power |
KIAS |
KTAS |
MPH
TAS |
| 1,500 |
2575 |
43 |
100 |
160 |
162 |
186 |
| 7,000 |
2575 |
43 |
100 |
155 |
165 |
190 |
| 17,000 |
2575 |
43 |
93 |
140 |
182 |
210 |
| 3,000 |
2400 |
33 |
75 |
120 |
126 |
145 |
| 17,000 |
2400 |
33 |
75 |
130 |
175 |
202 |
| 8,000 |
2200 |
30 |
65 |
130 |
147 |
170 |
| 10,000 |
2400 |
26 |
55 |
115 |
134 |
154 |
| 17,000 |
2000 |
26 |
50 |
115 |
154 |
177 |
aircraft
comparison chart
*Cessna U206G on wheels at
3800 lbs MGTOW
On Floats
Cruise Data**
Altitude
MSL |
Engine
RPM |
Manifold
Pressure |
%
Power |
KIAS |
KTAS |
MPH
TAS |
| 3,000 |
2300 |
34 |
75 |
- |
- |
140 |
| 5,000 |
2200 |
32 |
70 |
- |
- |
139 |
| 9,000 |
2200 |
30 |
65 |
- |
- |
165 |
| 10,000 |
2300 |
33 |
75 |
- |
- |
165 |
**Cessna U206G on Whipline amphibious
floats with flint tip tanks installed
disclaimer
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