SNCAC NC.510
SNCAC · France · first flew 1938 · reconnaissance aircraft
The SNCAC NC.510 was a twin-engine French reconnaissance, army co-operation or advanced training aircraft built in the late 1930s.
Recognition (WEFT)
| W — Wings | Mid-mounted, straight |
|---|---|
| E — Engines | 2 × piston, wing-mounted |
| F — Fuselage | 10.12 m fuselage |
| T — Tail | Twin fin |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Twin-engined mid-wing monoplane
- Crew of three
- Span of 15 m
A twin-engine mid-wing monoplane.
Specifications
- The SNCAC NC.510 has a length of 10.12 m (33 ft).
- It has a wingspan of 15 m (49 ft).
- Its maximum speed is 350 km/h (217 mph).
- Typical crew: 3.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew on 20 June 1938.
Variants
Three were built and refined.
Where you'll see it
Production orders were not forthcoming.
Related aircraft
- Farman NC.470
- SNCAC NC.130
- SNCAC NC.150
- SNCAC NC.4-10
- Aichi E12A
- Arado Ar 198
- Beriev MDR-5
- Blohm & Voss BV 141
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