Elements of Section - A4001 | ||
Area of Section |
0.264 in2 (1.7 cm2)
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Axis 1-1
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Axis 2-2
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Moment of Inertia (I) |
0.037 in4 (1.5 cm4)
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0.058 in4 (2.4 cm4)
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Section Modulus (S) |
0.058 in3 (1.0 cm3)
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0.093 in3 (1.5 cm3)
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Radius of Gyration (r) |
0.372 in (0.9 cm )
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0.469 in (1.2 cm )
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Beam Loading - A4001 | ||||||
Span (in) |
Max Allowable Uniform Load (lbs) |
Defl at Uniform load (in) |
Uniform Loading at Deflection |
Lateral Bracing Reduction Factor |
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Span /180 (lbs) |
Span /240 (lbs) |
Span /360 (lbs) |
||||
18 | *350 | 0.02 | *350 | *350 | *350 | 1.00 |
24 | *350 | 0.06 | *350 | *350 | *350 | 1.00 |
36 | 330 | 0.19 | 330 | 270 | 180 | 0.97 |
48 | 240 | 0.32 | 200 | 150 | 100 | 0.89 |
60 | 200 | 0.52 | 130 | 100 | 60 | 0.82 |
72 | 160 | 0.72 | 90 | 70 | 40 | 0.74 |
84 | 140 | 1.00 | 70 | 50 | 30 | 0.67 |
*Load limited by weld shear
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Notes:
- Above loads include the weight of the member. This weight must be deducted to arrive at the net allowable load the beam will support.
- Long span beams should be supported so as to prevent rotation and twist.
- Allowable uniformly distributed loads are listed for various simple spans, that is, a beam on two supports. If load is concentrated at the center of the span, multiply load from the table by 0.5 and corresponding deflection by 0.8.
- The lateral bracing factor should be multiplied by the load to determine the load retained based on the distance between lateral braces.
Part No. | Finish | Length | Weight | Box Qty. |
A4001
|
16
|
90.00
|
400
|
|
A4001
|
16
|
95.40
|
400
|
|
A4001
|
16
|
90.00
|
400
|
|
A4001
|
16
|
40.00
|
400
|