Breda Ba.75
Breda · Italy · first flew 1939 · reconnaissance aircraft
The Breda Ba.75 was an Italian prototype two-seat reconnaissance and ground-attack aircraft designed and built by the Societa Italiana Ernesto Breda.
Recognition (WEFT)
| W — Wings | Mid-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 11.3 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Two-seat mid-wing monoplane
- Single radial piston engine
- Reconnaissance and ground-attack role
Look for a two-seat mid-wing monoplane with a single radial engine.
Specifications
- The Breda Ba.75 has a length of 11.3 m (37 ft).
- It has a wingspan of 15.6 m (51 ft).
- Its maximum speed is 375 km/h (233 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew in 1939 and was powered by a radial piston engine.
Variants
There were no variants: only one aircraft was built.
Where you'll see it
The type did not enter production.
Related aircraft
- Breda Ba.201
- Breda Ba.88 Lince
- Breda Ba.65
- Breda Ba.44
- Aichi E13A
- Beriev MBR-7
- Bréguet 790 Nautilus
- Bristol Bolingbroke
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