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 Industria Aeronáutica Brasileira
First flight 1960s

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)

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References

Notes
  1. Orbis 1985, p. 2179
  2. 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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