IABSA Premier 64-01

From Wikipedia, the free encyclopedia
Jump to: navigation, search
Premier 64-01
Role Training or touring monoplane
National origin Brazil
Manufacturer Industria Aeronáutica Brasileira
First flight 1960s

The IABSA Premier 64-01 was a Brazillian two-seat training and touring monoplane designed and built in small numbers by Industria Aeronáutica Brasileira (IABSA).[1] Powered by a 75 hp (56 kW) piston engine, the Premier was a braced high-wing monoplane. [1]

Specifications[edit]

Data from Jane's All The World's Aircraft 1965–66[2]

General characteristics

  • Crew: 2
  • 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)
  • Cruising speed: 130 km/h (81 mph; 70 kn) (normal cruise)
  • Range: 600 km (373 mi; 324 nmi)
  • Service ceiling: 4,000 m (13,123 ft)

References[edit]

Notes[edit]

  1. ^ a b Orbis 1985, p. 2179
  2. ^ Taylor 1965, p. 12.

Bibliography[edit]