Cessna 210 Centurion
Piston • single engine • High Wing • Fixed gear
Range Visualization
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Payload vs. Range
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Default: 190 lbs (FAA standard)
Default: 30 lbs
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@ lbs / pax
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Fuel on board
gal
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Range
Available Range
/ nm
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( gal usable for nm range).
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Mission Profile
193
KTAS
Cruise Speed
6
Occupants
900
nm
Max Range
1175
lbs
Wet Payload
About the Cessna 210 Centurion
The Cessna 210 Centurion is a six-seat, high-performance, single-engined aircraft introduced in 1957. It was produced by Cessna until 1986 and featured various design changes over the years, including a wider and deeper fuselage, a cantilever wing, and improved avionics. The aircraft was offered in normally aspirated, turbocharged, and pressurized versions (denoted with a P, i.e. P210).
Technical Specifications
Dimensions
- Wingspan
- 36.8 ft
- Length
- 28.2 ft
- Height
- 9.7 ft
Weights
- Max Takeoff Weight
- 3,800 lbs
- Max Landing Weight
- 3,800 lbs
- Useful Load
- 1,697 lbs
- Fuel Capacity
- 87 gal
Performance
- Cruise Speed
- 193 KTAS
- Range
- 900 NM
- Service Ceiling
- 27,000 ft
- Rate of Climb
- 930 fpm
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