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Davis DA-2A


Designed by Leeon D. Davis the DA-2A was available as a plans or kit built aircraft through D2 Inc. of Bend, Oregon. It is of all metal construction and features an all-moving V tail which is set at an angle of 100 degrees. A child’s seat can be fitted behind the main seating.

N21TM                    c/n 112                          USA

2 seat light aircraft first flown in 1966

Engine: 90hp(67kW) Continental                                                                                                     Length: 17’10"(5.43m)                                                                                          Height: 5’5"(1.65m)Wingspan: 19’3"(5.87m)                                                                                                No.built: 80+ Range: 400 miles(644km)                                                               Cruising speed: 125mph(201kmh) Empty weight: 750lb(340kg)                                                   Maximum take-off weight: 1250lb(567kg)

Davis DA-2A

                                       N9055B                    c/n 200

Davis DA-2A

                                       N2366Q                    c/n 002

Davis DA-2A

N74066                      c/n 1                                  

 

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