|National origin||Soviet Union|
First flown on the 20 August 1936, the ANT-35 was a twin-engined all-metal low-wing monoplane with conventional landing gear with retractable mainwheels. The prototype was powered by two 597 kW (800 hp) Gnome-Rhone 14K radial engines which were later replaced with Tumansky M-85 engines, which were Gnome-Rhone 14K's built under license. An improved version, the ANT-35bis, was powered by two 746 kW (1,000 hp) Shvetsov M-62IR engines. The type entered service with Aeroflot from 1937 and later served as liaison and VIP transport aircraft after June 1941.
- Prototype with two 597 kW (800 hp) Gnome-Rhone 14K radial engines (later replaced with M-85s)
- Production variant with two 746 kW (1,000 hp) Shvetsov M-62IR engines, one prototype and nine production aircraft.
- Crew: two or three
- Capacity: ten (passengers)
- Wingspan: 20.80 m (68 ft 3 in)
- Powerplant: 2 × Shvetsov M-62IR, 746 kW (1,000 hp) each
- Maximum speed: 372 km/h (231 mph)
- Range: 1,640 km (1,019 miles)
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.