Riley Super P210
Piston • single engine • High Wing • Retractable gear
Range Visualization
Origin: · click map to move · nm at current load
Payload vs. Range
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Default: 190 lbs (FAA standard)
Default: 30 lbs
Mission Profile
- High-Performance
- Complex
- Pressurization
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 & Weights
- Length
- 28.2 ft
- Parking area (ft2)
- 1552.1 ft2
- 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
- Never-Exceed (Vne)
- 200 KIAS
- Max Structural Cruise (Vno)
- 167 KIAS
- Approach Speed
- 75 KIAS
- Stall, Clean (Vs1)
- 67 KIAS
- Range
- 925 NM
- Service Ceiling
- 23,000 ft
- Rate of Climb
- 945 fpm
Similar to the Riley Super P210
Beech Bonanza 36
Beech Bonanza 36 (Turbo)
Beech Bonanza A36
See how the Riley Super P210 stacks up against similar aircraft