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2. 6061 aluminium alloy - Wikipedia

   en.wikipedia.org/wiki/6061_aluminium_alloy

   ASTM B221: Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes; ASTM B308/308M: Standard Specification for Aluminum-Alloy 6061-T6 Standard Structural Profiles; ASTM B483: Standard Specification for Aluminum and Aluminum-Alloy Drawn Tube and Pipe for General Purpose Applications

3. Bushcaddy L-160 - Wikipedia

   en.wikipedia.org/wiki/Bushcaddy_L-160

   The aircraft fuselage is made with a frame of welded 6061-T6 aluminum square tubing, covered in 6061-T6 sheet. Its 36 ft (11.0 m) span wing employs V-struts with jury struts. The wing has an area of 189 sq ft (17.6 m 2) and flaps. It can accept four-stroke powerplants from 125 to 180 hp (93 to 134 kW). Cabin access is via two fold-up doors.

4. Bushcaddy L-164 - Wikipedia

   en.wikipedia.org/wiki/Bushcaddy_L-164

   The aircraft fuselage is made with a frame of welded 6061-T6 aluminum square tubing, covered in 6061-T6 sheet. Its 36 ft (11.0 m) span wing employs V-struts with jury struts. The wing has an area of 189 sq ft (17.6 m 2) and flaps.

5. Pterodactyl Ascender - Wikipedia

   en.wikipedia.org/wiki/Pterodactyl_Ascender

   Construction of all Pterodactyl aircraft was predominantly of anodized 6061-T6 aluminum tubing, braced with swaged steel cables supported by a king post and with a sewn Dacron sail for wing covering. Fittings to join the tubing were either extruded or made from sheet and bolted together. [2] [5]

6. Bushcaddy R-80 - Wikipedia

   en.wikipedia.org/wiki/Bushcaddy_R-80

   The aircraft is made from 6061-T6 aluminum sheet over a cage of welded aluminum square 6061-T6 aluminum tube. The tail boom is conventional semi-monocoque construction. The non-tapered planform wings have 6061-T6 ribs and spars and employ a NACA 4413 (mod) airfoil. The airfoil modification removes the undercamber on the bottom of the wing ...

7. Bushcaddy R-120 - Wikipedia

   en.wikipedia.org/wiki/Bushcaddy_R-120

   The aircraft is made from 6061-T6 aluminum sheet over a cage of welded aluminum square 6061-T6 aluminum tube. The tail boom is conventional semi-monocoque construction. The non-tapered planform wings have 6061-T6 ribs and spars and employ a NACA 4413 (mod) airfoil. The airfoil modification removes the undercamber on the bottom of the wing ...