Aircraft › Cessna › Cessna 210 Centurion › Cessna T210, P210 Turbo and Pressurized Centurion
Cessna T210, P210 Turbo and Pressurized Centurion
This page covers the turbocharged T210 and the pressurized P210, which all have a Continental TSIO-520 engine. The T210 is rated at 285 hp, later models at 310 hp, and the P210R and T210R at 325 hp. The P210N and P210R have a pressurized cabin. The weight and fuel here are those of the P210R, the last pressurized model: 4,100 pounds and 87 gallons of usable fuel in the standard tanks. Seats are four or six, so none is shown. Range, speed, ceiling and size are left blank, so the page has no drawing. The T210 has ICAO code T210 and the P210 has P210.
- Engines
- One piston engine in the nose: Continental TSIO-520 series (285 to 325 hp)
- Max takeoff weight
- 4,100 lb (1,860 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 T210, P210 |
Private aircraft show specs only. No flight data is shown for them.