S.84
Role Twin-engined airliner
National origin Italy
Manufacturer Savoia-Marchetti
First flight 1936
Number built 1

The Savoia-Marchetti S.84 was an Italian twin-engined airliner developed in Italy, from the three-engined Savoia-Marchetti S.73; only the prototype was completed and the designation was re-used for the Savoia-Marchetti SM.84.

Specifications (S.84 prototype)

Data from Italian Civil and Military aircraft 1930-1945 [1]

General characteristics

  • Crew: 4+
  • Capacity: 18 passengers, 269 kg (594 lb) of baggage and 519 kg (1,144 lb) of cargo and mail
  • Length: 19.8 m (65 ft 0 in)
  • Wingspan: 24 m (78 ft 9 in)
  • Empty weight: 5,987 kg (13,200 lb)
  • Gross weight: 9,480 kg (20,900 lb)
  • Powerplant: 2 × Gnome-Rhône 14Krsd 14-cylinder air-cooled radial piston engines, 670 kW (900 hp) each

Performance

  • Maximum speed: 350 km/h (220 mph, 190 kn) at 2,000 m (6,560 ft)
  • Cruise speed: 315 km/h (196 mph, 170 kn)
  • Range: 999 km (621 mi, 540 nmi)
  • Service ceiling: 7,798 m (25,584 ft)
  • Time to altitude: 4,000 m (13,120 ft) in 18 minutes

Notes

  1. ↑ Thompson, Jonathan W. (1963). Italian Civil and Military aircraft 1930-1945. USA: Aero Publishers Inc. ISBN 0-8168-6500-0. LCCN 63-17621.

References

Wikimedia Commons has media related to Savoia-Marchetti S.84.
  • Thompson, Jonathan W. (1963). Italian Civil and Military aircraft 1930-1945. USA: Aero Publishers Inc. ISBN 0-8168-6500-0. LCCN 63-17621.
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