Airmak J4 Explained

The Airmak J4 is an Italian ultralight and light-sport aircraft designed and produced by Airmak S.r.l. of Capua. The design's first flight was in early 2011. The aircraft is supplied complete and ready-to-fly.[1]

Design and development

The aircraft is produced by Airmak S.r.l., a joint venture between Rafaelle Violetti and Valter Proietti of OMA Sud. It is manufactured at OMA Sud's Italian facility. Production commenced in the middle of 2012.[1] [2]

The J4 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin accessed by doors, fixed tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft fuselage is made from welded steel tubing, with riveted aluminium tail and wings. Its 9.441NaN1 span wing has an area of 11.6m2, employs a custom Iannotta airfoil and mounts flaps. The standard engine used is the 1000NaN0 Rotax 912ULS four-stroke powerplant.[1] [3]

As of January 2017 the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.[4]

Operational history

Reviewer Marino Boric described the design in a 2015 review as "elegant".[1]

Notes and References

  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 24. Flying Pages Europe SARL, 2015.
  2. Web site: Chi Siamo. 9 January 2017. Airmak. https://web.archive.org/web/20170110020153/http://www.airmak.it/?page_id=73. 10 January 2017. dead.
  3. Web site: J4. 8 January 2017. Airmak. https://web.archive.org/web/20170109021517/http://www.airmak.it/?page_id=89. 9 January 2017. dead.
  4. Web site: SLSA Make/Model Directory. 8 January 2017. Federal Aviation Administration. 26 September 2016.