SIAI-Marchetti
SM.101
The SIAI‑Marchetti SM.101 was a compact two‑seat, low‑wing monoplane conceived by the Italian manufacturer SIAI‑Marchetti in the mid‑1930s. Development began in 1934 as a response to the Regia Aeronautica’s demand for a reliable trainer and light liaison aircraft that could operate from short, uneven fields. Powered by a 120‑horse‑power Alfa‑Romeo Cepheus inverted‑V engine, the SM.101 featured an all‑metal stressed‑skin structure, retractable main landing gear, and a sliding canopy that offered excellent visibility for both pilot and instructor. Its modest 10‑meter wingspan and low wing loading granted gentle stall characteristics and short‑runway performance, while a maximum speed of 220 km/h and a range of 750 km made it suitable for reconnaissance missions and courier duties. Only 34 examples were built before production shifted to the more powerful SM.102, but the SM.101 left a lasting influence on Italian aeronautical design. It demonstrated the practicality of metal construction in light aircraft and paved the way for post‑war trainers such as the SIAI‑Marchetti S.205, cementing its place as a modest but pivotal step in the evolution of European general aviation. Today a few well‑preserved examples survive in museums, reminding enthusiasts of Italy’s interwar ingenuity.
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Production & History
- First Flight
- 1947
Design & Classification
- Manufacturer
- SIAI-Marchetti
- Wikidata ID
- Q339432