The BFW M.23, (the M standing for its designer Willy Messerschmitt), was developed in response to a specification issued in 1929 by the German Aero Club for the
Ostpreussenflug (East Prussian Circuit) competition. The result was an improved version of the
M.19, with seating for two, and wings that could be folded for transport or storage. The M.23 was a small, conventional low-wing
cantilever monoplane. It had a fixed
undercarriage, the mainwheels mounted on a cranked axle, plus a tailskid. The
fin and
rudder assembly were broader and shorter than that of the M.19, though the shape varied with sub-type. A wide variety of engines were fitted, with power ranging from the 28 kW (38 hp)
ABC Scorpion two-cylinder motor to the 112 kW (150 hp) of the seven-cylinder
Siemens Sh 14a
radial. The first of three production variants, the M.23a used low-powered engines and had a very angular vertical tail. The M.23b had curved upper
fuselage decking and a more rounded tail and was produced with a large range of engines, both
inline and radial. The length depended slightly on the engine fitted. The final version, the M.23c had an enclosed
cockpit, the most powerful engines and was slightly larger (200 mm/8 in in span, around 500 mm/20 in in length) than the earlier variants. Its tail was again different, more rounded at the top and missing the
elevator cutaway of the earlier models. At least one M.23b appeared on floats. ==Operational history==