The KR-2 is a side by side two seat version of the single seat KR-1 which was designed by Kenneth Rand and which made its first flight in 1972. The KR-2T is a tandem two seat version. The KR-2S is a stretched version with a length of 15’10"(4.82m), a wingspan of 23’0"(7.01m) and a maximum take-off weight of 980lb(445kg). Plans were available to homebuilders from Rand Robinson Engineering Inc. of California. A KR-2T has been fitted with a small turboprop.

G-BLDN                   c/n 10913                       USA

2 seat light aircraft first flown in 1974

Engine: 90hp(67kW) VW                                                                                                              Length: 14’6"(4.42m)                                                                                            Height: 3’6"(1.07m)Wingspan: 20’8"(6.3m)                                                                                              No.built: 1000+ Range: 2000miles(3215km)                                                             Cruising speed: 170mph(272kmh) Empty weight: 440lb(200kg)                                                     Maximum take-off weight: 800lb(363kg)

N5304J                   c/n 5240                                

A KR-2S with tricycle undercarriage is illustrated below.

N886MJ                 c/n 9425-886                            

A KR-2 with tricycle undercarriage is illustrated below.