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Cessna
Stationair

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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

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