title: SNCAC NC.860
text: # SNCAC NC.860
  
  The SNCAC NC.860 (also known as the Aérocentre NC.860) was a French twin-engined development of the NC.853 light aircraft.
  
  ## Development
  
  The NC.860 was developed from the earlier NC.853 single-engined high-wing monoplane, major changes included a four-seat cabin and the fitting of two 105 hp (78 kW) Walter Minor 4-III engines on a re-designed wing. With the engines mounted on the high-wing the wing span was increased and the NC.860 had a tricycle landing gear.
  
  The NC.860, registered F-WFKJ, first flew 28 March 1949.
  
  ## Specification
  
  Data from
  
  General characteristics
  
  * Crew: 1
  * Capacity: 3
  * Length: 7.7 m (25 ft 3 in)
  * Wingspan: 13.42 m (44 ft 0 in)
  * Wing area: 20.0 $m^2$ (215 sq ft)
  * Empty weight: 760 kg (1,676 lb)
  * Gross weight: 1,200 kg (2,646 lb)
  * Powerplant: 2 × Walter Minor 4-III four-cylinder inverted inline air-cooled engine, 78 kW (105 hp) each
  
  Performance
  
  * Maximum speed: 240 km/h (150 mph, 130 kn)
  * Cruise speed: 210 km/h (130 mph, 110 kn)
  * Range: 1,000 km (620 mi, 540 nmi)
  