Riley Super P210
Piston • single engine • High Wing • Retractable 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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Fuel on board
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Range
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Mission Profile
200
KTAS
Cruise Speed
6
Occupants
925
nm
Max Range
1034
lbs
Wet Payload
About the Riley Super P210
The Cessna P210 Pressurized Centurion is a single-engine, six-seat, pressurized high-wing aircraft with retractable gear, produced by Cessna 1978–1985. It’s powered by a 310 hp Continental TSIO-520-AF turbocharged engine, cruises at 200 ktas, climbs at 945 fpm to a service ceiling of 23 000 ft, stalls clean at 67 KIAS, and carries 90 US gal of fuel for a max range of 925 nm.
Technical Specifications
Dimensions
- Wingspan
- 36.75 ft
- Length
- 28.2 ft
- Height
- 9.7 ft
Weights
- Max Takeoff Weight
- 4,000 lbs
- Max Landing Weight
- 3,800 lbs
- Useful Load
- 1,574 lbs
- Fuel Capacity
- 90 gal
Performance
- Cruise Speed
- 200 KTAS
- Range
- 925 NM
- Service Ceiling
- 23,000 ft
- Rate of Climb
- 945 fpm
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