Introductions:

The Savoia-Marchetti S.73 was an Italian three-engine airliner that flew in the 1930s and early 1940s. The aircraft entered service in March 1935 with a production run of 48 aircraft. Four were exported to Belgium for SABENA, while seven others were produced by SABCA. The main customer was the Italian airline Ala Littoria.

The aircraft was developed in only four months, thanks to the use of the S.55 wing, combined with a much more conventional fuselage. Developed in parallel with a bomber version (the SM.81 Pipistrello) the prototype S.73 first flew on 4 June 1934 from Cameri, with Adriano Bacula as test pilot.

The prototype had a four-blade wooden propeller on the central engine, and two-blade wooden propellers on each wing engine. Later all aircraft were fitted with three-blade metal propellers.

The S.73 was a mixed-construction (a skeleton of steel covered by wood and fabric for the fuselage, wood for the three-spar wing) monoplane with a braced tailplane and fixed undercarriage. There were two generators, one in each side of the fuselage; the batteries were 24 V and were rated at 90 A.

The pilot and co-pilot were seated side-by-side in an enclosed cockpit, with a compartment for a radio operator and a mechanic. A passenger compartment could house 18 passengers in two rows.

It had eight metallic fuel tanks, all in the wings, with a total capacity of 3,950 L (1,040 US gal; 870 imp gal). The prototype had French Gnome-Rhône 9Kfr Mistral engines, but further aircraft had 522 kW (700 hp) Piaggio Stella P.X, 574 kW (770 hp) Wright R-1820, 544 kW (730 hp) Walter Pegasus III MR2V, Alfa Romeo 125 or Alfa Romeo 126, driving ground adjustable, three-bladed, aluminium-steel propellers.

It could be used from small airports, had reliable handling and was not too costly. With the 574 kW (770 hp)Wright R-1820 engine the S.73 had cruise/max speeds of 270?/?340 km/h (150?/?180 kn; 170?/?210 mph), 1,000 km (620 mi) range, and 6,300 m (20,700 ft) ceiling. With the 544 kW (730 hp) AR.126 the S.73 had a maximum speed of 345 km/h (186 kn; 214 mph), 1,000 km (620 mi) range, and 7,000 m (23,000 ft) ceiling. The SABCA license-produced aircraft had 671 kW (900 hp) Gnome-Rhône 14K Mistral Major engines for a total of 2,013 kW (2,699 hp), comparable to the last models of S.79s or the CANT Z.1018.

The S.73 had an unremarkable flight test programme with few modifications recommended by the Regia Aeronautica. It was easy to fly, rugged, and easy to operate on the ground, including the ability to fly from short airfields in treacherous terrain, in spite of being under-powered and the lack of leading edge slats. Its mixed construction and fixed landing gear were its main shortcomings, when contemporary aircraft in the US and Germany were of all-metal construction with retractable undercarriages. Some of these had better performance, but the S.73 remained competitive for some years.

Mentions:

JP11 for the wonderful images screenshots

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