S.84
General information
Type	Twin-engined airliner
National origin	Italy
Manufacturer	Savoia-Marchetti
Number built	1
History
First flight	1936

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.

Contents

• Specifications (S.84 prototype)
• Notes
• References

Specifications (S.84 prototype)

Data fromItalian 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

References

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