Korean Air Chang-Gong 91

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Chang-Gong 91
Role Four-seat light monoplane
National origin South Korea
Manufacturer Korean Air Aerospace Division
First flight 22 November 1991

The Korean Air Chang-Gong 91 (English: Blue Sky 91) is a four-seat single-engined low-wing monoplane designed by the Korea Institute of Aeronautical Technology[1] and built by the Aerospace Division of Korean Air.[2]

Specifications[edit]

Data from [2]

General characteristics

  • Crew: 1
  • Capacity: 3
  • Length: 7.74 m (25 ft 5 in)
  • Wingspan: 10.2 m (33 ft 5 in)
  • Height: 2.7 m (8 ft 10 in)
  • Wing area: 14.86 m2 (160 ft2)
  • Empty weight: 839 kg (1850 lb)
  • Gross weight: 1225 kg (2700 lb)
  • Powerplant: 1 × Lycoming IO-360-A1B6 piston engine, 149 kW (200 hp)

Performance

  • Maximum speed: 339 km/h (210 mph)
  • Range: 1500 km (932 miles)
  • Service ceiling: 5025 m (16,500 ft)

See also[edit]

Aircraft of comparable role, configuration and era

References[edit]

Notes[edit]

  1. ^ "Korean industry makes show debut". Flight International: 13. 1989-08-26. 
  2. ^ a b Taylor 1996, p.408

Bibliography[edit]

  • Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.