SIAI-Marchetti

SM.1019

The SIAI‑Marchetti SM.1019 is an Italian light utility aircraft that first flew in 1969 and entered service in the early 1970s. Developed from the earlier SM.1017 agricultural plane, the aircraft was built to meet the Italian Army’s requirement for a short‑take‑off and landing (STOL) liaison and observation platform. Powered by a single Lycoming IO‑540‑D4A5 six‑cylinder engine delivering 260 hp, the low‑wing monoplane features a fixed tricycle undercarriage, high‑mounted flaps and leading‑edge slats that give it a take‑off run of less than 300 m and a payload capacity of around 600 kg. The cockpit is equipped with dual controls, a transparent nose and panoramic windows that provide excellent visibility for reconnaissance, medical evacuation and cargo transport. Over 200 SM.1019s were produced, serving not only the Italian forces but also several foreign air forces and civilian operators. Its robust construction, simple maintenance requirements and excellent STOL performance made it a versatile workhorse in rugged environments, influencing later light‑utility designs and cementing SIAI‑Marchetti’s reputation for practical, cost‑effective aircraft. During the 1980s the SM.1019 was adapted for aerial fire‑suppression, fitted with a 200‑litre water tank, showing its civilian versatility. Today examples remain in museum collections, preserving the legacy of design that combined simplicity, capability and flexibility.

Classification

Dimensions

Length
335.5 inch
Height
49.25 inch
Wingspan
24.75 inch
Mass
2800 pound

Performance

Maximum Speed
135 knot

Production & History

First Flight
1969

Design & Classification

Country of Origin
Manufacturer
SIAI-Marchetti
Engine
Allison 250-B15G
Wikidata ID
Q1247989