IABSA Premier 64-01
The IABSA Premier 64-01 was a Brazilian two-seat training and touring braced high-wing monoplane designed and built in small numbers by Industria Aeronáutica Brasileira (IABSA),[1] powered by a 75 hp (56 kW) piston engine.[1]
| Premier 64-01 | |
|---|---|
| Role | Training or touring monoplane |
| National origin | Brazil |
| Manufacturer | Indústria Aeronáutica Brasileira |
| Designer | Vicente Martin Llopis |
| First flight | 1964 |
| Number built | 1 |
Specifications
Data from Jane's All The World's Aircraft 1965–66[2]
General characteristics
- Crew: two
- Length: 6.70 m (22 ft 0 in)
- Wingspan: 10.70 m (35 ft 1 in)
- Wing area: 16.0 m2 (172 sq ft)
- Empty weight: 340 kg (750 lb)
- Max takeoff weight: 580 kg (1,279 lb)
- Fuel capacity: 70 L (15 imp gal; 18 US gal)
- Powerplant: 1 × Continental A75 air-cooled four-cylinder horizontally-opposed engine, 56 kW (75 hp)
- Propellers: 2-bladed McCauley 1A90 fixed pitch metal propeller
Performance
- Maximum speed: 160 km/h (99 mph, 86 kn)
- Cruise speed: 130 km/h (81 mph, 70 kn) (normal cruise)
- Range: 600 km (370 mi, 320 nmi)
- Service ceiling: 4,000 m (13,000 ft)
References
Notes
- Orbis 1985, p. 2179
- Taylor 1965, p. 12.
Bibliography
- Taylor, John W. R. (1965). Jane's All The World's Aircraft 1965–66. London: Sampson Low, Marston & Company, Ltd.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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