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6063 grade is commonly referred to as the architectural alloy. It was developed as an extrusion alloy with relatively high tensile properties, excellent finishing characteristics and a high degree of resistance to corrosion. This alloy is most often found in various interior and exterior architectural applications, such as windows, doors, store fronts and assorted trim items. It is the alloy best suited for anodizing applications - either plain or in a variety of colors.

6063-T52
Stock Lengths 16'
(Sharp Inside and Outside Corners)
AMS-QQ-A-200/9
Metal & Alloy Structural Tees & Zees
Unit of Measure
Items Metal & Alloy Structural Tees & Zees
6063-T52T-750-750-125
Aluminum Architectural Tees - Series 6063
Metal & Alloy Structural Tees & Zees
6063-T52T-1000-1000-125
Aluminum Architectural Tees - Series 6063
Metal & Alloy Structural Tees & Zees
6063-T52T-1250-875-125
Aluminum Architectural Tees - Series 6063
Metal & Alloy Structural Tees & Zees
6063-T52T-2000-750-125
Aluminum Architectural Tees - Series 6063
Material N/A Aluminum
Shapeform N/A Architectural Tees
Series N/A 6063-T52
Grade N/A 6063
Temper N/A T52
Size N/A 3/4 x 3/4 x 1/8 inches N/A 1 x 1 x 1/8 inches N/A 1 1/4 x 7/8 x 1/8 inches N/A 2 x 3/4 x 1/8 inches
Working Decimal Equivalent N/A 0.750 x 0.750 x 0.125 inches19.05 x 19.05 x 3.175 mm N/A 1.000 x 1.000 x 0.125 inches25.4 x 25.4 x 3.175 mm N/A 1.250 x 0.875 x 0.125 inches31.75 x 22.225 x 3.175 mm N/A 2.000 x 0.750 x 0.125 inches50.8 x 19.05 x 3.175 mm
Dimension A N/A 3/4 inches N/A 1 inches N/A 1 1/4 inches N/A 2 inches
Dimension B N/A 3/4 inches N/A 1 inches N/A 7/8 inches N/A 3/4 inches
Thickness N/A 1/8 inches
Estimated Weight N/A 0.1998 lbs/ft0.2973351672 kg/m N/A 0.2716 lbs/ft0.4041853424 kg/m N/A 0.2910 lbs/ft0.433055724 kg/m N/A 0.3822 lbs/ft0.5687762808 kg/m
Estimated Weight per 25' Bar N/A 3.197 lbs1.448241 kg N/A 4.346 lbs1.968738 kg N/A 4.656 lbs2.109168 kg N/A 6.115 lbs2.76783 kg
ASTM Specification N/A AMS-QO-A-200/9
Stock Length N/A 16 ft
Ultimate Strength N/A 27 ksi
Yield Strength N/A 21 ksi
Elongation percent in 2 inches N/A 12
Hardness Brinnel Number N/A 60
Ultimate Shearing Strength N/A 17 ksi
Fatigue Endurance Limit1 N/A 10 ksi
Modulus of Elasticity2 N/A 10.0 x 103 ksi
Resistance to Corrosion - General3 N/A A
Stress Corrosion Cracking N/A A
Workability (Cold) N/A B
Mechinability N/A C
Brazeability4 N/A A
Gas Weldability5 N/A A
Arc Weldability6 N/A A
Resistance Spot and Seam Weldability7 N/A A
Applications N/A Pipe railing, furniture, architectural extrusions
Density N/A 0.097 lbs/inĀ³
Specific Gravity N/A 2.70
  • 1 Based on 500,000.000 cycles of completely reversed stress using the R. R. Moore-type of machine and specimen.
  • 2 Average of tension and compression moduli. Compression modulus is about 2 percent greater than tension modulus.
  • 3 Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D and E ratings generally should be protected at least on faying surfaces.
  • 4 Ratings A through D for Weldability and Brazeability are relative ratings.
  • 5 A = Generally weldable by all commercial procedures and methods.
    B = Weldable with special techniques or for specific applications that justify preliminary trials or testing to develop welding procedure and weld performance.
    C = Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
  • 6 A = Generally weldable by all commercial procedures and methods.
    B = Weldable with special techniques or for specific applications that justify preliminary trials or testing to develop welding procedure and weld performance.
    C = Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
  • 7 A = Generally weldable by all commercial procedures and methods.
    B = Weldable with special techniques or for specific applications that justify preliminary trials or testing to develop welding procedure and weld performance.
    C = Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.