span wing employs

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  • The aircraft's span wing employs a single strut per side.
  • Its span wing employs ailerons on the lower wing only.
  • Like most Jodel designs its span wing employs dihedral in the outer half only.
  • Its span wing employs a single strut per side.
  • Its span wing employs a large wing area of to produce a low wing loading to allow the aircraft to make use of small and light sources of lift.
  • Its span wing employs flaps and is supported by V-struts with jury struts.
  • Its span wing employs a dual spar design with V-struts and jury struts.
  • The span wing employs polyhedral configuration with the outer wing panels exhibiting much greater dihedral.
  • Its span wing employs a Clark Y airfoil, has an area of and optional flaps.
  • Its span wing employs an A315 airfoil, has an area of and utilizes flaperons.
  • Its span wing employs Fowler flaps to keep the stall speed low enough for the FAI microlight category.
  • Its span wing employs a USA 35B airfoil, has an area of and mounts flaps.
  • Its span wing employs a modified Clark Y airfoil.
  • Its span wing employs a Carbon-fiber-reinforced polymer spar and carbon sandwich construction.
  • Its span wing employs V-struts with jury struts.
  • Its span wing employs V-struts and jury struts.
  • Its span wing employs an NN-1817 airfoil, has an area of and flaps.
  • Its span wing employs a NACA 2412 mod airfoil, has an area of and large flaps.
  • Its span wing employs an American-designed NACA 4415 airfoil.
  • Its span wing employs "V" lift struts and jury struts.
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