Savoia-Marchetti S.84

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 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

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

References

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

Aircraft produced by SIAI, Savoia-Marchetti and SIAI-Marchetti

SIAI	S.8 S.9 S.12 S.13 S.16 S.17 S.19 S.21 S.22 S.23 S.50 S.51 S.52 S.58 S.67

Marchetti	MVT

Savoia-Marchetti	S.55 S.56 S.57 S.59 SM.62 S.64 S.65 S.66 S.71 S.72 S.73 SM.74 SM.75 SM.76 SM.77 S.78 SM.79 SM.80 SM.81 SM.82 SM.83 S.84 SM.84 SM.85 SM.86 SM.87 SM.88 SM.89 SM.90 SM.91 SM.92 SM.93 SM.94 SM.95

SIAI-Marchetti	SM.101 SM.102 SA.202 S.205 S.208 S.210 S.211 SF.260 SF.600 S.700 SM.1019

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