page_title: De Havilland Dragon
section_title: Specifications (DH.84 Dragon 1)
hierarchical_section_title: De Havilland Dragon / Specifications (DH.84 Dragon 1)
caption_attribution_description: English: De Havilland DH 84 3-view drawing from L'Aerophile February 1933
context_page_description: The de Havilland DH.84 Dragon is a successful small commercial aircraft that was designed and built by the de Havilland company.
context_section_description: Data from de Havilland Aircraft since 1909
  General characteristics
  Crew: 1
  Capacity: 6–10 passengers
  Length: 34 ft 6 in (10.52 m)
  Wingspan: 47 ft 4 in (14.43 m)
  Height: 10 ft 1 in (3.07 m)
  Wing area: 376 sq ft (34.9 m²)
  Airfoil: RAF 15
  Empty weight: 2,300 lb (1,043 kg)
  Gross weight: 4,200 lb (1,905 kg)
  Powerplant: 2 × de Havilland Gipsy Major I 4-cylinder air-cooled inverted in-line piston engine, 130 hp (97 kW)  each
  Propellers: 2-bladed fixed-pitch propellers
  Performance
  Maximum speed: 128 mph (206 km/h, 111 kn)
  Cruise speed: 109 mph (175 km/h, 95 kn)
  Range: 460 mi (740 km, 400 nmi)
  Service ceiling: 12,500 ft (3,800 m)
  Rate of climb: 612 ft/min (3.11 m/s)
caption: De Havilland DH 84 3-view drawing from L'Aerophile February 1933
exif: {}