|National origin||Soviet Union|
|First flight||1 September 1934|
The I-17 was a lightweight single-seat low-wing cantilever monoplane. Developed under the design bureau designation TsKB-15 it first flew on 1 September 1934 powered by a 567 kW (760 hp) Hispano-Suiza 12 Ybrs engine. The second prototype designated the TsKB-19 had a revised inward retracting wide-track main landing gear and a Soviet M-100 engine. This second prototype was displayed at the 1936 Salon de l'Aeronautique in Paris. The third prototype designated the TsKB-33 had reduced armament to save weight and a revised engine cooling system, but the further development was abandoned in 1936.
A number of related unbuilt projects were also under development including the I-17Z parasite fighter under the designations TsKB-25 with a M-34RNF engine and the TsKB-43 with a Hispano-Suiza engine, none were built.
- First prototype I-17 powered by a 567 kW (760 hp) Hispano-Suiza 12 Ybrs engine.
- Second revised I-17 prototype powered by a M-100 engine.
- Unbuilt I-17Z project for a Mikulin AM-34RNF powered parasite fighter.
- Third revised I-17 prototype with reduced armament.
- Unbuilt project with a Hispano-Suiza engine.
- Crew: 1 (pilot)
- Length: 7.30 m (23 ft 11 in)
- Wingspan: 10.19 m (33 ft 5 in)
- Height: 2.56 m (8 ft 5 in)
- Gross weight: 1,930 kg (4,250 lb)
- Powerplant: 1 × Klimov M-100 engine, 632 kW (860 hp) each
- Maximum speed: 490 km/h (305 mph)
- Range: 800 km (497 miles)
- Service ceiling: 11,000 m (36,090 ft)
- Angelucci, Enzo (1980). The Rand McNally Encyclopedia of Military Aircraft. Rand McNally Publishing. p. 183.
- Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875-1995. London: Osprey. ISBN 1-85532-405-9.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
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