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Cessna 210 Centurion
This page covers the normally aspirated Centurion, from the 210 of 1959 to the 210R. The first models have a Continental IO-470 of 260 hp, and the later ones an IO-520 of 285 hp, with 300 hp for takeoff on the 210K and later. Maximum weights run from 2,900 to 3,850 pounds and seats are four or six. The weight and fuel here are those of the 210R, the last model: 3,850 pounds and 87 gallons of usable fuel in the standard tanks. Seats, range, speed, ceiling and size are left blank, so the page has no drawing.
- Engines
- One piston engine in the nose: Continental IO-470 series (260 hp) and IO-520 series (285 to 300 hp)
- Max takeoff weight
- 3,800 lb (1,746 kg)
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Specifications
| Fuselage width | 4 ft 1 in (1.25 m) |
|---|---|
| Fuel capacity | 90 US gal (329 L) |
| Status | In service |
| Type codes | ICAO C210 |
Private aircraft show specs only. No flight data is shown for them.