Putilov Stal-3
Putilov · Soviet Union · first flew 1933 · transport aircraft
The Stal-3 (Stal meaning steel) was a transport aircraft designed and built in the USSR from 1933.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 10.68 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- High-wing monoplane transport
- Single M-22 radial engine
- Cabin for six or seven passengers
A single-engined high-wing monoplane 10.68 m long with a 17.02 m span.
Specifications
- The Putilov Stal-3 has a length of 10.68 m (35 ft).
- It has a wingspan of 17.02 m (56 ft).
- Typical crew: 1-2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed by A. I. Putilov and developed from the Putilov Stal-2. It first flew in 1933.
Variants
It was developed from the Stal-2. 79 Stal-3 aircraft were built.
Where you'll see it
It carried one or two crew and six or seven passengers, and was powered by a 480 hp M-22 engine with a range of 940 km.
Related aircraft
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