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  2. SIAI-Marchetti S.211 - Wikipedia

    en.wikipedia.org/wiki/SIAI-Marchetti_S.211

    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 ...

  3. SIAI-Marchetti - Wikipedia

    en.wikipedia.org/wiki/SIAI-Marchetti

    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 ...

  4. Aermacchi M-345 - Wikipedia

    en.wikipedia.org/wiki/Aermacchi_M-345

    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.

  5. Joint Primary Aircraft Training System - Wikipedia

    en.wikipedia.org/wiki/Joint_Primary_Aircraft...

    Northrop Super Tucano EMB-312H – an improved EMB-312 Tucano with uprated engine and other improvements. Grumman S.211A a modified SIAI Marchetti S.211. Rockwell Ranger 2000 based on the RFB Fantrainer. Vought Pampa 2000 – a modified FMA IA 63

  6. List of aircraft (Si) - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft_(Si)

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Help; Learn to edit; Community portal; Recent changes; Upload file

  7. SIAI-Marchetti S.210 - Wikipedia

    en.wikipedia.org/wiki/SIAI-Marchetti_S.210

    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.

  8. SIAI-Marchetti S.205 - Wikipedia

    en.wikipedia.org/wiki/SIAI-Marchetti_S.205

    The prototype SIAI S.205 exhibited at the Paris Air Show in June 1965 S.205 basic version, metal, single-engine four-seat airplane, the F version had a fixed undercarriage, while the R version had a retractable undercarriage. It was offered with three different engines: S.205 F/R-18: Avco Lycoming O-360 S.205 F/R-20: Avco Lycoming IO-360-A1A

  9. SIAI-Marchetti SF.260 - Wikipedia

    en.wikipedia.org/wiki/SIAI-Marchetti_SF.260

    In 1991–1992, SIAI-Marchetti proposed an updated SF.260, with an enlarged cockpit canopy and a revised fuel system to meet the United States Air Force's Enhanced Flight Screener competition. While the bid was unsuccessful (with the Slingsby T67 Firefly being preferred), it formed the basis for future production, as the fuel injected SF.260E ...