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Aerospace Spot Weld Shear Strength: aluminum alloy

alum ftu above56 t0020 to alum ftu above56 t0160

Design-allowable shear load per spot (lbs) for resistance spot welds per MIL-HDBK-5J Section 8.2.2.3 and MIL-W-6858. Indexed by material family (aluminum alloy, steel/nickel/cobalt alloy, magnesium alloy, titanium alloy), parent metal Ftu range (ksi), and sheet thickness (in). Tensile allowable is 25% of shear strength. Covers thicknesses 0.020–0.160 in. No filler metal — allowable is empirical load-per-spot based on sheet thickness and parent metal ultimate tensile strength.

Aerospace Engineeringmaterial family: aluminum alloy10 rowsPage 2 of 3
material familyrecord iddesign shear strength lbs (lbf)material ftu range ksisheet thickness in (in)standardtensile allowable lbs (lbf)tensile allowable noteweld spec
aluminum alloyalum ftu above56 t002068above 560.02MIL-HDBK-5J Section 8.2.2.31725% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t002596above 560.025MIL-HDBK-5J Section 8.2.2.32425% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0032140above 560.032MIL-HDBK-5J Section 8.2.2.33525% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0040196above 560.04MIL-HDBK-5J Section 8.2.2.34925% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0050276above 560.05MIL-HDBK-5J Section 8.2.2.36925% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0063396above 560.063MIL-HDBK-5J Section 8.2.2.39925% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0080536above 560.08MIL-HDBK-5J Section 8.2.2.313425% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0100720above 560.1MIL-HDBK-5J Section 8.2.2.318025% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t0125920above 560.125MIL-HDBK-5J Section 8.2.2.323025% of shear strengthMIL-W-6858
aluminum alloyalum ftu above56 t01601,296above 560.16MIL-HDBK-5J Section 8.2.2.332425% of shear strengthMIL-W-6858

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