The SNCAC NC.4-10 was a twin-engined floatplane torpedo bomber built in France in the late 1930s, one of several prototypes competing for a French Navy specification, and no contracts were awarded after the military lost interest. It began as the Farman F.410, designed in 1934 before the part-nationalisation of 1936 and 1937 brought Farman and Hanriot together as SNCAC, and was revised to meet the MT/CPT-9 specification for a combat scout seaplane. It was an all-metal aircraft with low-set wings, twin fins on the tailplane, a largely glazed nose and long floats, armed with three machine guns and a cannon. It first flew on 10 July 1939 with two Gnome-Rhône 14K radials of 890 horsepower, later replaced by 1,050 horsepower 14N engines, and flew as a floatplane from September 1939.
Facts
Engine Class Top Speed (km/h) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source SNCAC NC.4-10 (Wikipedia)
Of Make
Source SNCAC NC.4-10 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source SNCAC NC.4-10 (Wikipedia)Design and development, originQuote, Design and development, origin
The Farman F.410 was designed in 1934, before the part-nationalisation of the French aircraft industry in 1936-7 brought Farman and Hanriot together
Originated In
Also in Geography Atlas: where this subject originated.
Source SNCAC NC.4-10 (Wikipedia)Lead, typeQuote, Lead, type
The SNCAC NC.4-10 was a twin-engine floatplane torpedo bomber built in France in the late 1930s.
Sources
1. SNCAC NC.4-10 (Wikipedia)
Design and development, first flight
When the NC.4-10 first flew, piloted by Lucian Coupet on 10 July 1939
Lead, type
The SNCAC NC.4-10 was a twin-engine floatplane torpedo bomber built in France in the late 1930s.
Design and development, engines
it was powered instead by a pair of 890 hp (635 kW) Gnome-Rhône 14Knrs/ors 14-cylinder radials
Specifications, powerplant
Powerplant: 2 × Gnome-Rhône 14Knrs/ors 14-cylinder, two row radial, 660 kW (890 hp) each
Specifications, power per engine
Powerplant: 2 × Gnome-Rhône 14Knrs/ors 14-cylinder, two row radial, 660 kW (890 hp) each
Specifications, maximum speed
Maximum speed: 326 km/h (203 mph, 176 kn)
Design and development, origin
The Farman F.410 was designed in 1934, before the part-nationalisation of the French aircraft industry in 1936-7 brought Farman and Hanriot together
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