page_title: De Havilland Flamingo
section_title: Specifications (de Havilland Flamingo)
hierarchical_section_title: De Havilland Flamingo / Specifications (de Havilland Flamingo)
caption_attribution_description: Polski: DH 95 Flamingo - rzuty
context_page_description: The de Havilland DH.95 Flamingo was a British twin-engined high-wing monoplane airliner first flown on 22 December 1938. During the Second World War some were used by the Royal Air Force as a transport and general communications duties.
context_section_description: Data from De Havilland Aircraft since 1909
  General characteristics
  Crew: 3
  Capacity: 17 passengers
  Length: 51 ft 7 in (15.72 m)
  Wingspan: 70 ft 0 in (21.34 m)
  Height: 15 ft 3 in (4.65 m)
  Wing area: 651 sq ft (60.5 m²)
  Empty weight: 11,325 lb (5,137 kg)
  Gross weight: 18,000 lb (8,165 kg)
  Powerplant: 2 × Bristol Perseus XVI 9-cylinder air-cooled sleeve-valve radial piston engines, 930 hp (690 kW)  each
  Propellers: 3-bladed variable-pitch propellers
  Performance
  Maximum speed: 243 mph (391 km/h, 211 kn)
  Cruise speed: 204 mph (328 km/h, 177 kn)
  Range: 1,345 mi (2,165 km, 1,169 nmi)
  Service ceiling: 20,900 ft (6,400 m)
  Rate of climb: 1,470 ft/min (7.5 m/s)
  Avionics
  Sperry Automatic Pilot
caption: De Havilland Flamingo
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