These leaned outwards at the front and rear of the wing, the latter supplemented with a central, transverse inverted V-pair.

The fin and rudder were also smoothly curved together; the latter extended to the keel and worked in a rounded elevator cut-out.

A short V-form strut was attached to each lower fuselage longeron, joined by a cross-piece at their apexes, above which a single axle bearing the main wheels was rubber sprung.

[1] Though the results were satisfactory and although it met the requirements set by the Romanian Ministry for War,[1] no orders for serial production were received.

[2] Data from Les Ailes June 1925,[1] Romanian Aeronautical Constructions 1905 - 1974[2]General characteristics Performance