Putilov Stal-2
OOS · Soviet Union · first flew 1931 · airliner
The Stal-2 was a Russian mid-range passenger aircraft designed by A. I. Putilov.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 9.74 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- High-wing single-engined monoplane
- Mid-range passenger aircraft seating four
- Powered by an M-26 or MG-31 engine of 300 hp
It is a high-wing single-engined monoplane carrying a pilot and four passengers.
Specifications
- The Putilov Stal-2 has a length of 9.74 m (32 ft).
- It has a wingspan of 16.2 m (53 ft).
- Its maximum speed is 200 km/h (124 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew on 11 October 1931. It was built by OOS and later at GAZ-81.
Variants
The Putilov Stal-3 was a variant of the Stal-2.
Where you'll see it
Aeroflot was the primary user. 111 had been built by 1935.
Related aircraft
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