Neha Patil (Editor)

Korean Air Chang Gong 91

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Top speed
  
339 km/h

Length
  
7.74 m

Wingspan
  
10 m

First flight
  
November 22, 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 and built by the Aerospace Division of Korean Air.

Specifications

Data from

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)

    • References

    Korean Air Chang-Gong 91 Wikipedia
    (Text) CC BY-SA


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