page_title: Sikorsky S-35
section_title: Specifications
hierarchical_section_title: Sikorsky S-35 / Specifications
caption_attribution_description: English: Sikorsky S-35 3-view drawing from Les Ailes June 24, 1926
context_page_description: The Sikorsky S-35 was an American twin-engined sesquiplane transport later modified to use three-engines. It was designed and built by the Sikorsky Manufacturing Company for an attempt by Rene Fonck on a non-stop Atlantic crossing for the Orteig Prize. It was destroyed in the attempt.
context_section_description: Data from Best
  General characteristics
  Crew: four
  Length: 44 ft 0 in (13.41 m)
  Upper wingspan: 101 ft 0 in (30.78 m)
  Lower wingspan: 76 ft 0 in (23.16 m)
  Height: 16 ft 0 in (4.88 m)
  Wing area: 794 sq ft (73.8 m²) upper wing
  Empty weight: 9,700 lb (4,400 kg)
  Gross weight: 20,000 lb (9,072 kg)
  Max takeoff weight: 24,200 lb (11,000 kg)
  Powerplant: 3 × Gnome-Rhône Jupiter 9A radial engine, 425 hp (317 kW)  each
  Propellers: 2-bladed, 10 ft 6 in (3.20 m) diameter
  Performance
  Maximum speed: 145 mph (233 km/h, 126 kn)
  Endurance: 7 hours
  Service ceiling: 16,800 ft (5,100 m)
caption: Sikorsky S-35 3-view drawing from Les Ailes June 24, 1926
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