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]
^Sport Aviation: 49. March 1975. {{cite journal}}: Missing or empty |title= (help)
^Flight International. 22 August 1977. {{cite journal}}: Missing or empty |title= (help)
January 01, 1970
rand, robinson, american, amphibious, aircraft, that, designed, rand, role, homebuilt, aircraft, national, origin, united, states, designer, rand, introduction, 1977, contents, design, development, specifications, also, referencesdesign, development, editthe, . The Rand Robinson KR 3 is an American amphibious aircraft that was designed by Ken Rand 1 KR 3 Role Homebuilt aircraft National origin United States Designer Ken Rand Introduction 1977 Contents 1 Design and development 2 Specifications KR 3 3 See also 4 ReferencesDesign and development editThe 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 editData from Flight InternationalGeneral characteristicsCrew 1 Capacity 1 passenger Powerplant 1 Volkswagen air cooled engine horizontally opposed piston PerformanceSee also editRelated development Rand Robinson KR 1 Aircraft of comparable role configuration and era Icon A5References edit Sport Aviation 49 March 1975 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Flight International 22 August 1977 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Retrieved from https en wikipedia org w index php title Rand Robinson KR 3 amp oldid 1066442639, wikipedia, wiki, book, books, library,
