Samiksha Jaiswal (Editor)

IABSA Premier 64 01

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Top speed
  
160 km/h

Length
  
6.7 m

Wingspan
  
11 m

First flight
  
1960

Manufacturer
  
Industria Aeronáutica Brasileira

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), powered by a 75 hp (56 kW) piston engine.

Specifications

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

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 (373 mi; 324 nmi)
  • Service ceiling: 4,000 m (13,000 ft)

    • References

    IABSA Premier 64-01 Wikipedia
    (Text) CC BY-SA