Savoia-Marchetti engineers took the basic three-engine design with its low-set monoplane wings and modernized it in the hopes of a better product. The fuselage was revised and uprated engines installed. The original wings were retained and the cockpit flightdeck remained in stepped position over the long nose assembly. The tail unit consisted of a dual-vertical tail fin arrangement and the undercarriage was of a "tail-dragger" configuration. Armor protection for the crew and systems were improved over that of the "softer" SM.79 series and self-sealing fuel tanks were used. Construction included a steel tube understructure with metal skin and fabric at the fuselage while the wings were of wood. The fuselage housed an internal bomb bay.
A prototype was developed and this recorded its first flight on June 5th, 1940. After the requisite flight testing phase, the aircraft was ordered into production by December and formally introduced during 1941 as the "SM.84". It was intended to succeed the aging SM.79 series in full.
The three-engine concept allowed for additional pulling power without a major disruption of the overall design. Several well-known tri-engined aircraft were used throughout the war including Ford's famous Tri-Motor as well as the recognizable contribution by Junkers with its Ju 52.
As completed, the SM.84 featured a crew of up to six - pilots, radioman, engineer, bombardier, and machine gunners. Dimensions included a length of 18 meters with a wingspan of 21 meters and height of 4.6 meters. Empty weight was listed at 19,500lbs with a loaded weight nearing 29,330lbs. Power was served through 3 x Piaggio P.XI RC 40 14-cylinder, air-cooled radial piston engines - one fitted at the nose and the other two along each wing leading edge as normal. Output was 1,000 horsepower each which allowed for a maximum speed of 270 miles per hour with a range out to 1,140 miles and a service ceiling of 25,920 feet.
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