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Falconar F-11A


Another plans-built design from Falconar, the F-11A is a modified Jodel D.11. The F-11E, first flown in 1987.

Falconar F-11A N9293

N9293                      c/n 8019                     Canada

2 seat light aircraft first flown in 1968

Engine: 85hp(63kW) Continental                                                                                                    Length: 22’0"(6.7m)                                                                                              Height:6’4"(1.92m)Wingspan: 27’3"(8.29m)                                                                                                No.built: 40+ Range: 546miles(876km)                                                                 Cruising speed: 130mph(208kmh) Empty weight: 715lb(324kg)                                                   Maximum take-off weight: 1300lb(590kg)

Illustrated below is a lighter version with a maximum take-off weight of 1100lb(499kg).

Falconar F-11E C-GFST

                                  C-GFST                       c/n E.6515

 

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