| 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.
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Transcription
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
- ^ 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.
This page was last edited on 31 January 2023, at 12:28