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EN AW-7475

EN AW-7475
aluminum7xxx_al_zn
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High-purity damage-tolerant Al-Zn-Mg-Cu alloy — controlled Fe+Si (<0.22% total) for maximum fracture toughness. T7351: UTS 490-530 MPa with KIc ~33 MPa√m (vs ~26 for 7075-T6). THE alloy for fatigue-critical fuselage skins where crack growth rate matters most. Used for lower wing skins, fuselage skins of wide-body aircraft (Boeing 747/777), and any primary structure requiring damage tolerance.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸AAUSAAA 7475 / UNS A97475A97475REF
🇪🇺ENEuropeEN AW-7475 / AlZn5.5MgCuEN AW-7475100%

Sources: AA, EN 573-3

Chemical composition comparison (wt%)

Side-by-side: EN AW-7475 (EN 573-3) vs EN AW-7475 / AlZn5.5MgCu (EN) (EN 573-3)

ElementEN AW-7475 (EN 573-3)EN AW-7475 / AlZn5.5MgCu (EN)Overlap
Si0–0.1%
Cr0.18–0.25%

Mechanical properties

Compatibility verdict

EN AW-7475 and EN AW-7475 / AlZn5.5MgCu: 100% composition match

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