CSS-12
Centralne Studium Samolotow · Poland · first flew 1950 · airliner
The CSS-12 was a prototype Polish twin-engined feederliner of the 1950s.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 2 × piston, wing-mounted |
| F — Fuselage | 12.5 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Twin-engined low-wing monoplane
- Two Argus As 411 engines
- Wingspan of 18.5 m
A twin-engined low-wing airliner prototype.
Specifications
- The CSS-12 has a length of 12.5 m (41 ft).
- It has a wingspan of 18.5 m (61 ft).
- Its maximum speed is 365 km/h (227 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
A single example was built and first flew on 22 November 1950.
Variants
There were no variants: only one was built.
Where you'll see it
No production followed.
Related aircraft
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