The Nuri Demirağ Nu D.36 was a 1930s Turkish two-seat training biplane built by the Nuri Demirağ Aircraft Works in Istanbul for the Turkish military.
== Design == The Nu D.36 is an unequal-span single-bay staggered biplane with a fixed conventional landing gear with a tailskid. It was powered by a 150 hp (112 kW) Walter Gemma I nine-cylinder radial engine. It had two open tandem cockpits for the pilot and trainee.
== Operators == Turkey Turkish Air Force
== Specifications == Data from Jane's Fighting Aircraft of World War II, Jane's all the World's Aircraft 1947General characteristics Crew: 2 Length: 7.3 m (23 ft 11 in) Wingspan: 9.74 m (31 ft 11 in) Height: 2.44 m (8 ft 0 in) Wing area: 21.8 m2 (235 sq ft) Empty weight: 650 kg (1,433 lb) Max takeoff weight: 1,000 kg (2,205 lb) Powerplant: 1 × Walter Gemma I 9-cyl. air-cooled radial piston engine, 110 kW (150 hp) Propellers: 2-bladed fixed pitch wooden propeller Performance
Maximum speed: 182 km/h (113 mph, 98 kn)with maximum load <--*Landing speed: 85 km/h (53 mph; 46 kn) (commented out as this does not work in wikitext) -->
Range: 500 km (310 mi, 270 nmi) Endurance: 3 hours 30 minutes Service ceiling: 3,350 m (10,990 ft) Time to altitude: 500 m (1,600 ft) in 2 minutes; 1,500 m (4,900 ft) in 10 minutes