Cessna

Cessna P210R Pressurized Centurion

The Cessau P210R Pressurized Centurion, produced by Cessna Aircraft Company from 1972 until 1985, represents a pivotal step in the evolution of high‑performance, single‑engine, pressurized aircraft. Derived from the earlier P210 model, the R variant incorporated a strengthened airframe, a larger 300‑horsepower Continental TSIO‑520‑N engine, and an improved cabin pressurization system that maintained a comfortable 8,000‑foot equivalent altitude while cruising at 30,000 feet. Its retractable tricycle landing gear, all‑metal construction, and sleek, low‑drag wing design gave it a cruise speed of roughly 227 knots and a range of over 1,000 nautical miles, making it attractive to both corporate operators and air‑taxi services.

Historically, the P210R filled the niche between light twins such as the Beechcraft Baron and larger twin‑engine pressurized transports, demonstrating that a single engine could safely and efficiently fly at high altitude with passenger comfort. The aircraft’s reliability, relatively low operating costs, and ability to operate from short runways contributed to its popularity in the 1970s and early 1980s. Though production ended in 1985, the Centurion remains a respected classic, often prized by owners for its blend of speed, altitude capability, and economic operation.
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Design & Classification

Manufacturer
Cessna
Wikidata ID
Q15830897