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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 ...
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
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.
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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.
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The Nardi FN.333 Riviera, later the SIAI-Marchetti FN.333 Riviera, is an Italian luxury touring amphibious aircraft designed and developed by Fratelli Nardi in the 1950s and produced in small numbers by Savoia-Marchetti during the following decade. On October 25, 1968, FN-333, Serial # 007 was destroyed in an accident at Akron Municipal Airport.