In today's article we want to explore the fascinating world of Tecnam Astore. From its emergence to its impact on current society, Tecnam Astore has been the subject of focus and debate in different areas. Throughout this article, we will examine its evolution over time, as well as its many facets and its influence on different aspects of life. In addition, we will analyze its relevance in the current context and its potential for the future. Tecnam Astore is a fascinating topic that never ceases to surprise us, and through this article we hope to shed new light on its importance and meaning in our lives.
Astore | |
---|---|
Prototype Astore | |
Role | Light-sport aircraft |
National origin | Italy |
Manufacturer | Tecnam |
Designer | Luigi Pascale |
First flight | June 2013[1] |
Status | In production |
Produced | 2013-present |
Number built | 30 (2014) |
The Tecnam Astore (English: Goshawk) is an Italian, low wing, two-seater, light-sport aircraft, under development by Tecnam of Naples. It was first flown in early June, 2013, and introduced at the AERO Friedrichshafen show in 2013. It is supplied complete and ready-to-fly.[1][2]
The Astore replaced the Tecnam P2002 Sierra in ultralight production, although not the certified P2002JF model.[2]
The aircraft was designed to comply with the US Light Sport Aircraft (LSA) rules. It features a cantilever low-wing, two seats in side-by-side configuration, an enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.[1][2][3]
The aircraft is made from aluminum sheet. Its wing has a span of 8.65 m (28.4 ft) and is equipped with flaps. Standard engines available are the 100 hp (75 kW) Rotax 912ULS and 912iULS, plus the 115 hp (86 kW) Rotax 914 four-stroke powerplants.[2][3]
The Astore achieved its FAA LSA compliance in April 2014. More than thirty had been delivered by September 2014.[4]
Reviewer Marino Boric described the design in a 2015 review as "beautiful".[2]
Data from AOPA, Pew and Tecnam [1][3][5]
General characteristics
Performance
Avionics