Partenavia Alpha
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The Partenavia P.70 Alpha was a 1970s Italian two-seat light aerobatic trainer designed by Luigi Pascale and built by Partenavia.
Design and development
The Alpha was a low-wing monoplane with a fixed tricycle landing gear and powered by a 100hp (75kW) Rolls-Royce Continental O-200-A engine. The Alpha first flew on the 24 April, 1972, but only one was built and it did not enter production as the company was pre-occupied with producing the Partenavia P.68.
Specifications
Data from Jane's All the World's Aircraft 1973-74
General characteristics
- Crew: 2
- Length: 7.06m (23ft 2in)
- Wingspan: 8.5m (27ft 11in)
- Height: 3.00m (9ft 10in)
- Wing area: 11.60m2 (125sqft)
- Empty weight: 480kg (1,014lb)
- Gross weight: 700kg (1,543lb)
- Powerplant: 1 × Rolls-Royce Continental O-200-A four-cylinder horizontallt-opposed air-cooled piston engine , 75kW (100hp)
Performance
- Maximum speed: 225km/h (140mph, 120kn)
- Cruise speed: 210km/h (130mph, 110kn)
- Range: 880km (546mi, 474nmi)
- Service ceiling: 4,000m (13,125ft)
- g limits: +6 -3
- Rate of climb: 4.00m/s (787ft/min)
Notes
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
- Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing. ISBN1-85310-194-X.
- Taylor, John W.R., ed. (1973). Jane's All the World's Aircraft 1973-74. London, United Kingdom: Jane's Yearbooks. ISBN0-354-00117-5.