Korean Air Chang-Gong 91
| Korean Air Chang-Gong 91 | |
|---|---|
| Type: | Light aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
November 22, 1991 |
| Number of pieces: |
1 prototype |
The Korean Air Chang-Gong 91 is a light touring aircraft produced by the Korean manufacturer Korean Air Aerospace Division .
History and construction
The Chang-Gong 91 was developed at the Korea Institute of Aeronautical Technology and built by the Korean Air Aerospace Division . The machine is designed as a low-wing aircraft and has a non-retractable nose wheel landing gear. Access to the cabin is provided by two doors above the wings, which are located on the right and left. The machine is driven by a Lycoming IO 360 A1B6 boxer engine with 149 kW. Only a prototype should have been built.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| Passengers | 3 |
| length | 7.70 m |
| span | 10.20 m |
| height | 2.70 m |
| Wing area | 14.86 m² |
| Empty mass | 680 kg |
| Max. Takeoff mass | 1,225 kg |
| Cruising speed | 232 km / h |
| Top speed | 241 km / h |
| Service ceiling | 4,420 m or ft |
| Range | 1,500 km |
| Engines | 1 × Lycoming-IO-360 -A1B6 boxer engine with 149 kW |
See also
Preserved copies
- The prototype is in the Korean Air Museum on Jeju Island
literature
- Jane's All The World's Aircraft 1991-92, ISBN 978-0-7106-0965-6
Web links
- Data and images from doc8643.com (en) accessed on May 8, 2016
- KOREAN AIR AEROSPACE DIVISION website (s) accessed on May 8, 2016
Individual evidence
- ^ "Korean industry makes show debut". Flight International: August 13-26, 1989
- ↑ Jane's All The World's Aircraft 1991-92, ISBN 978-0-7106-0965-6
- ↑ Data and images from doc8643.com (en) accessed on May 8, 2016