Korean Air Chang-Gong 91

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

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

Aircraft of comparable role, configuration and era

• KAI KC-100 Naraon - later South Korean light aircraft project
  

References

Notes

Bibliography

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