General aviation composites: From fairings to fuselages

Market forecaster Chris Red sketches general aviation's long history with composites.


Facebook Share Icon LinkedIn Share Icon Twitter Share Icon Share by EMail icon Print Icon

General aviation (GA) has had a long history with composites. Many of the platforms included in this market outlook feature advanced composites in flight-control surfaces and some empennage skins, as well as aerodynamic fairings around the wings and stabilizers. These applications represent from 6 percent to 20 percent of an aircraft’s airframe.

The aircraft’s fuselage and wings each roughly account for 35 percent of the remaining airframe mass. Although GA manufacturers as a group are currently more conservative in their use of composites in primary structures, individual manufacturers were among the first to produce all-composite airframes. These included the Lear Avia (now the Learjet subsidiary of Bombardier Aerospace, Dorval, Quebec, Canada) Learfan 2100 in the early 1980s and the Hawker Beechcraft (Wichita, Kan.) Starship later in that decade. Only a few all-composite aircraft are included in this forecast, but a growing number of OEMs are finding it competitively advantageous to convert fuselages and other major subassemblies from aluminum to composites. On many of these aircraft, composite materials account for 50 percent to as much as 65 percent of the total airframe weight. Although composites continue to penetrate the GA structural materials market, it is important to note that an aluminum fuselage and wing are still the norm, rather than the exception, in GA manufacturing.

Related Topics


  • Out-of-autoclave prepregs: Hype or revolution?

    Oven-cured, vacuum-bagged prepregs show promise in production primary structures.

  • Boeing 787 Update

    Approaching rollout and first flight, the 787 relies on innovations in composite materials and processes to hit its targets

  • Fabrication methods

    There are numerous methods for fabricating composite components. Selection of a method for a particular part, therefore, will depend on the materials, the part design and end-use or application. Here's a guide to selection.