Form This specification covers an aluminum alloy in the form of sheet and plate 0.009 to 1.000 inch (0.23 to 25.40 mm)@ inclusive@ in nominal thickness (see 8.5). Application These products have been used typically for parts requiring moderate forming and where good welding characteristics and resistance to corrosion are important@ but usage is not limited to such applications.
SAE AMS4017L-2018 history
2024SAE AMS4017M-2024 Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened, Half-Hard, and Stabilized
2018SAE AMS4017L-2018 Aluminum Alloy Sheet and Plate 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened@ Half-Hard@ and Stabilized (UNS A95052)
2017SAE AMS4017K-2017 Aluminum Alloy Sheet and Plate 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened, Half-Hard, and Stabilized
2004SAE AMS4017K-2004 Aluminum Alloy, Sheet and Plate, 2.5Mg 0.25Cr, (5052-H34), Strain-Hardened, Half-Hard, and Stabilized
1995SAE AMS4017J-1995 ALUMINUM ALLOY SHEET AND PLATE 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened, Half-Hard, and Stabilized
1995SAE AMS4017-1995 ALUMINUM ALLOY SHEET AND STRIP Magnesium Chromium (52S-1/2H)
1991SAE AMS4017J-1991 Aluminum Alloy, Sheet and Plate, 2.5Mg 0.25Cr, Strain-Hardened, Half-Hard, and Stabilized (Reaffirmed: 01 May 1995)
1989SAE AMS4017H-1989 ALUMINUM ALLOY SHEET AND PLATE@ 2.5Mg - 0.25Cr (5050-H34) Strain-Hardened@ Half-Hard@ and Stabilized (UNS A95052)