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Aerospace Spot Weld Shear Strength: aluminum alloy

alum ftu below38 t0020 to alum ftu below38 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 3 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 below38 t002048below 380.02MIL-HDBK-5J Section 8.2.2.31225% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t002568below 380.025MIL-HDBK-5J Section 8.2.2.31725% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t003296below 380.032MIL-HDBK-5J Section 8.2.2.32425% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0040136below 380.04MIL-HDBK-5J Section 8.2.2.33425% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0050192below 380.05MIL-HDBK-5J Section 8.2.2.34825% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0063276below 380.063MIL-HDBK-5J Section 8.2.2.36925% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0080376below 380.08MIL-HDBK-5J Section 8.2.2.39425% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0100504below 380.1MIL-HDBK-5J Section 8.2.2.312625% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0125644below 380.125MIL-HDBK-5J Section 8.2.2.316125% of shear strengthMIL-W-6858
aluminum alloyalum ftu below38 t0160880below 380.16MIL-HDBK-5J Section 8.2.2.322025% of shear strengthMIL-W-6858

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