Rand-Robinson KR-3
| KR-3 | |
|---|---|
| Role | Homebuilt aircraft | 
| National origin | United States | 
| Designer | Ken Rand | 
| Introduction | 1977 | 
The Rand-Robinson KR-3 is an American amphibious aircraft that was designed by Ken Rand.[1]
Design and development
The KR-3 is a two-seat composite construction amphibious aircraft. The landing gear is hydraulically retractable. The prototype was demonstrated at the EAA airshow in 1977, demonstrating water taxi tests.[2]
Specifications (KR-3)
Data from Flight International
General characteristics
- Crew: 1
 - Capacity: 1 passenger
 - Powerplant: 1 × Volkswagen air-cooled engine horizontally opposed piston
 
Performance
See also
Related development
Aircraft of comparable role, configuration, and era