The Nuri Demirağ Nu.D.38 was a Turkish light civil transport, with twin engines and seating for four passengers, built in the early 1940s.

Design work on the Nu.D.38 twin engine light transport began about 1936[2] and the aircraft was largely completed by 1941,[1] but the first flight was delayed until 1944.

[5] The fuselage of the Nu.D.38 was an oval cross-section aluminium alloy monocoque, with stressed skin over frames and longitudinal stringers.

[5] The Nu.D.38 was powered by two 160 hp (120 kW) Bramo Sh 14-A4 radial engines, mounted to the main wing spar on steel frames.

A main shock absorber leg was attached to each of the steel engine frames, braced rearwards by a short auxiliary strut.