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6061-T6 aluminium standard heat treating process. T6 temper 6061 has been treated to provide the maximum precipitation hardening (and therefore maximum yield strength) for a 6061 aluminium alloy. It has an ultimate tensile strength of at least 290 MPa (42 ksi) and yield strength of at least 240 MPa (35 ksi).
It has a masthead sloop rig with 6061-T6 aluminum spars, a raked stem, a vertical transom, a skeg-mounted rudder controlled by an Edson-built wheel and a centerboard with stub keel or optional fixed fin keel in deep or shoal lengths. It displaces 7,500 lb (3,402 kg) and carries 3,500 lb (1,588 kg) of ballast. [1] [3] [7] [4]
Plywood coring is employed for the cabin top, deck, seat and the cockpit sole for stiffness. The hull-to-deck joint is flanged, glued and then screwed into place. There is an aluminum toe rail, stainless steel through-bolted into place, bonding the toe rail, deck and the hull. [2] The spars are all coated 6061-T6 aluminum extrusions. There is a ...
The AlMgSi alloys are therefore understood in the standards as a separate group (6000 series) and not as a subgroup of aluminum-magnesium alloys that cannot be hardenable. AlMgSi is one of the aluminum alloys with medium to high strength, high fracture resistance, good welding suitability, corrosion resistance and formability. They can be ...
The four most common aluminium grades available as sheet metal are 1100-H14, 3003-H14, 5052-H32, and 6061-T6. [5] [7] Grade 1100-H14 is commercially pure aluminium, highly chemical and weather resistant. It is ductile enough for deep drawing and weldable, but has low strength.
The engine had electric start and the craft had fiberglass composite spring landing gear. Airframe construction was bolted 6061-T6 aluminum thin-wall tube, with 6061 T-6 extruded angle. The craft took off, flew, and landed at around 30 mph. [30]