Pitcairn PCA-2 Civil Aircraft Model Details

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General Information of Pitcairn PCA-2

Designer : Harold F. Pitcairn

First Flight : 1931

Manufacturer : Pitcairn-Cierva Autogiro Company

National Origin : United States

Number Built : 20–30

Role : Utility autogyro

General characteristics of Pitcairn PCA-2

Capacity : 2 passengers

Crew : One pilot

Empty Weight : 2,233 lb (1,015 kg)

Gross Weight : 3,000 lb (1,363 kg)

Length : 23 ft 1 in (7.04 m)

Main Rotor Area : 1,590 ft2 (147 m2)

Main Rotor Diameter : 45 ft 0 in (13.72 m)

Powerplant : 1 × Wright R-975-J6-9, 330 hp (250 kW)

Wingspan : 30 ft 0 in (9.14 m)

Performance of Pitcairn PCA-2

Maximum Glide Ratio : 4.8[11]

Maximum Speed : 120 mph (190 km/h)

Range : 290 miles (466,7 km)

Service Ceiling : 15,000 ft (4,575 m)

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