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"SM.84
Some confusion resulted from the designation SM.84, originally applied in 1935 to a twin engined transport. later, during the war, the number was given to a three-engined bomber developed from the SM.79 Sparviero.
The civil transport, while bearing a general similarity to the Douglas DC-3 and no doubt influenced by it, was actually an eighteen-passenger twin-engined development of the SM.73. Powered by 900 h.p. Gnome-Rhone 14 Krsd fourteen-cylinder radial engines, the SM.84 weighed 13,200 lb. empty and 20,900 lb. loaded, including 594 lb. of baggage and 1144 lb. of cargo and mail. Performance included a maximum speed of 220 m.p.h. at 6560 ft., a cruising speed of 196 m.p.h., and a landing speed of 57 m.p.h. Service ceiling was 25,584 ft. and range 621 miles. The SM.84 transport climbed to 13,120 ft. in 18 min. Dimensions were: span 78 ft. 8 3/4 in., length 64 ft. 11 1/3 in., height 15 ft. 7 in., and wing area 1000.7 sq. ft. The airliner never went into production."