page_title: Armstrong Whitworth Argosy
section_title: Specifications (Argosy II)
hierarchical_section_title: Armstrong Whitworth Argosy / Specifications (Argosy II)
caption_attribution_description: English: Armstrong Whitworth Argosy 3 view drawing from NACA Aircraft Circular No.14
context_page_description: The Armstrong Whitworth Argosy was a British three-engine biplane airliner built by Armstrong Whitworth Aircraft, and operated by Imperial Airways from 1926 to 1935.
context_section_description: General characteristics
  Crew: 2
  Capacity: 20 passengers
  Length: 64 ft 6 in (19.66 m)
  Wingspan: 90 ft 0 in (27.43 m)
  Height: 19 ft 0 in (5.79 m)
  Wing area: 1,890 sq ft (176 m²)
  Empty weight: 12,090 lb (5,484 kg)
  Max takeoff weight: 19,200 lb (8,709 kg)
  Powerplant: 3 × Armstrong Siddeley Jaguar IVA 14-cylinder radial engines, 420 hp (310 kW)  each
  Performance
  Maximum speed: 110 mph (180 km/h, 96 kn)
  Cruise speed: 90 mph (140 km/h, 78 kn)
  Range: 405 mi (652 km, 352 nmi)
  Time to altitude: 4.5 min to 3,000 ft (910 m)
caption: Armstrong Whitworth Argosy 3 view drawing from NACA Aircraft Circular No.14
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