LIBIS KB-11
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| KB-11 Branko | |
|---|---|
| Type | Four-seat light trainer and tourer |
| Manufacturer | |
| Designed by | Letalski Institut Branko Ivanus Solvenija |
| Maiden flight | 1959 |
The LIBIS KB-11 Branko was a 1950s Yugoslavian four-seat monoplane designed by Letalski Institut Branko Ivanus Solvenija.
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[edit] Design and development
The aircraft design office of the Letalski Institut Branko Ivanus Solvenija brought together teachers and students of the Ljubljana technical high school. The KB-11 Branko was a development of the earlier two-seat KB-6 Matajur. First flown in December 1959 the KB-11 was a cantilever low-wing monoplane with retractable tricycle landing gear and an enclosed heated and ventilated cockpit for four persons. Intended for use as an air-taxi our business use but only small numbers were built.
[edit] Specifications (KB-11)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Capacity: Four
- Powerplant: 1 × Avco Lycoming O-435-1 flat-six piston, 185 kW (134 hp)
Performance
- Maximum speed: 245 km/h (152 mph)
- Range: 950 km (590 miles)
[edit] References
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
[edit] External links
[edit] See also
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