Savoia-Marchetti S.84
S.84 | |
---|---|
Role | Twin-engined airliner |
National origin | Italy |
Manufacturer | Savoia-Marchetti |
First flight | 1936 |
Number built | 1 |
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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 pax, 269 kg (594 lb) of baggage and 519 kg (1,144 lb) of cargo and mail
- Length: 19.79506 m (64 ft 11.333 in)
- Wingspan: 23.9967 m (78 ft 8.75 in)
- Empty weight: 5,987 kg (13,200 lb)
- Gross weight: 9,480 kg (20,900 lb)
- Powerplant: 2 × Gnome-Rhône 14Krsd 14 cyl. air-cooled radial piston engines, 670 kW (900 hp) each
Performance
- Maximum speed: 354 km/h; 191 kn (220 mph) at 2,000 m (6,560 ft)
- Cruise speed: 315 km/h; 170 kn (196 mph)
- Range: 999 km; 540 nmi (621 mi)
- 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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