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The S-211's single JTI5D-4C engine provides a maximum thrust output of 11.12 kN (2,500 lbs) and a specific fuel consumption of 0.57 lb/h/lb. [8] This powerplant facilitates a maximum speed of 414 knots at 25,000 ft and a rate of climb of 5,100 ft per minute. Fuel is housed internally within both the integral wing tank and a bladder cell within ...
SIAI-Marchetti S.208 – 5-seat version of S.205 (1967) SIAI-Marchetti S.210 – twin-engined cabin aircraft (1970) SIAI-Marchetti S.211 – two-seat jet trainer, light attack aircraft (1981) SIAI-Marchetti S.226 – 22 passenger business jet project (1980s) SIAI-Marchetti S.229 – swept-wing canard twin engine jet aircraft project, enlarged ...
It is a development of the SIAI-Marchetti S.211. On 29 December 2016, the M-345 performed its maiden flight; one month later, the first order for the type was placed by the Italian Air Force. The first production-standard M-345 was flown from Venegono Superiore in December 2018; and entered service in December 2020 replacing MB-339.
Download as PDF; Printable version; In other projects Wikidata item; Appearance. move to sidebar hide. ... SIAI-Marchetti S.211; SIAI-Marchetti S.205; SIAI-Marchetti ...
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The S.210 was developed from the single-engined S.205 and was an all-metal low-wing cantilever monoplane with a retractable tricycle landing gear. It was powered by two 200 hp (149 kW) Avco Lycoming TIO-360 -A1B engines, one mounted on the leading edge of each wing.
Although the S.50 did not meet the specifications the Regia Aeronautica (Italian Royal Air Force) had established for entrants in the 1923 single-seat fighter contest—which specified that entrants be powered by the 224-kilowatt (300-horsepower) Hispano-Suiza HS 42 eight-cylinder water-cooled engine [3] —SIAI entered it anyway.
To meet an Italian Army requirement for a short take-off liaison aircraft, SIAI-Marchetti modified the design of the Cessna 305A/O-1 Bird Dog with a new turboprop engine and a revised tail unit. The prototype first flew on 24 May 1969 powered by a 317 hp (236 kW) Allison 250-B15C turboprop engine.