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