page_title: Farman F.140 Super Goliath
section_title: Specifications (F.140)
hierarchical_section_title: Farman F.140 Super Goliath / Specifications (F.140)
caption_attribution_description: English: Farman F.140 Super Goliath 3-view drawing from Les Ailes February 26, 1926
context_page_description: The Farman F.140 Super Goliath was a very large, four engine biplane night bomber, designed in France in the mid-1920s. Nine flew with the French Air Force until concerns about structural weakness grounded them in 1930. The prototype set several world records for altitude reached with heavy useful loads.
context_section_description: Data from Les Avions Farman
  General characteristics
  Crew: 6
  Length: 19.70 m (64 ft 8 in)
  Wingspan: 31.40 m (103 ft 0 in)
  Height: 6.50 m (21 ft 4 in)
  Wing area: 241.00 m² (2,594.1 sq ft)
  Empty weight: 7,705 kg (16,987 lb)
  Gross weight: 11,792 kg (25,997 lb)
  Powerplant: 4 × Farman 12We W-12 (three banks of 4 cylinders) water-cooled, 370 kW (500 hp)  each
  Propellers: 4-bladed Levasseur
  Performance
  Maximum speed: 182 km/h (113 mph, 98 kn)
  Range: 450 km (280 mi, 240 nmi)
  Service ceiling: 6,500 m (21,300 ft)
  Time to altitude: 26 min 19 s to 4,000 m (13,123 ft)
  Armament
  Bombs: 3,000 kg (6,610 lb)
caption: Farman F.140 Super Goliath 3-view drawing from Les Ailes February 26, 1926
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