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SNCAC NC.4-10

Flying Boats and Seaplanes

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
Year
1939 1
Engine Class
Piston 1
Power (kW)
660 1
Top Speed (km/h)
326 1
Engine
Gnome-Rhone 14Knrs/ors 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source SNCAC NC.4-10 (Wikipedia)

Of Make

Source SNCAC NC.4-10 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source SNCAC NC.4-10 (Wikipedia)Design and development, origin
Quote, 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, type
Quote, 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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