The Dobi-II is the second airplane designed by Lithuanian aviator Jurgis Dobkevičius in 1922. It was tested in October 1923. After two landing accidents plans for mass production of Dobi-II were abandoned.
The Dobi-II had long ailerons and were able to be folded due to an internal mechanism. This was most likely done to reduce storage, as the Dobi-II was intended for military usage. During the 1923's the Dobi-II was one of the fastest planes among the two seat aircraft with 200 hp engines. Additionally the hanging control column was used in the Dobi-II. 
Specifications.
"Data from" Lithuanian Air MuseumGeneral characteristics* Crew: 2* Aspect ratio: * Propellers: -bladed
Performance* Endurance: * g limits: * Roll rate: * Maximum glide ratio: * Time to altitude: 34 min to*Landing speed: 
References.
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