page_title: Norman Aviation Nordic VII
section_title: Specifications (Nordic VII)
hierarchical_section_title: Norman Aviation Nordic VII / Specifications (Nordic VII)
caption_attribution_description: English: Norman Aviation Nordic VII advanced ultralight aircraft at Les Faucheurs de Marguerites, Sherbrooke, Quebec, Canada.
context_page_description: The Norman Aviation Nordic VII is a Canadian advanced ultralight aircraft, that was designed by Jacques Norman and produced by Norman Aviation of Saint-Anselme, Quebec. The aircraft was supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.
  Production is complete and the Nordic VII is no longer available.
context_section_description: Data from Purdy
  General characteristics
  Crew: one
  Capacity: one passenger
  Length: 20.17 ft (6.15 m)
  Wingspan: 33.80 ft (10.30 m)
  Wing area: 135 sq ft (12.5 m²)
  Empty weight: 625 lb (283 kg)
  Gross weight: 1,058 lb (480 kg)
  Fuel capacity: 12 U.S. gallons (45 L; 10.0 imp gal)
  Powerplant: 1 × Subaru EA engine four cylinder, air-cooled, four stroke automotive engine, 100 hp (75 kW)
  Propellers: 2-bladed composite
  Performance
  Maximum speed: 115 mph (185 km/h; 100 kn)
  Cruise speed: 105 mph (169 km/h; 91 kn)
  Stall speed: 40 mph (64 km/h; 35 kn)
  Range: 350 mi (304 nmi; 563 km)
  Service ceiling: 10,000 ft (3,000 m)
  Rate of climb: 500 ft/min (2.5 m/s)
  Wing loading: 7.8 lb/sq ft (38 kg/m²)
caption: Norman Aviation Nordic VII
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