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 sq ft)
- Empty weight: 839 kg (1,850 lb)
- Gross weight: 1,225 kg (2,700 lb)
- Powerplant: 1 × Lycoming IO-360-A1B6 piston engine , 149 kW (200 hp)
Performance
- Maximum speed: 339 km/h (210 mph, 180 kn)
- Range: 1,500 km (932 mi, 810 nmi)
- Service ceiling: 5,025 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
