Filler Metal, Aluminum Brazing, 12Si
Copper-Beryllium Alloy, Bars and Rods, 98Cu - 1.9Be, Solution and Precipitation Heat Treated (TF00, formerly AT)
Copper-Beryllium Alloy, Bars, Rods, Shapes, and Forgings, 98Cu - 1.9Be, Solution Heat Treated TB00 (A)
Heat Treatment of Wrought Aluminum Alloy Parts
Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged
This sheet has been used typically for structural parts requiring good strength, toughness, and fatigue properties and maximum corrosion resistance, but usage is not limited to such applications.
Aluminum Sheet, Laminated, Surface Bonded
Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024, -T3 Sheet/-T351 Plate with 1½% Alclad) Solution Heat Treated, Cold Worked and Naturally Aged (Composition similar to UNS A82024)
This specification covers an aluminum alloy in the form of sheet and plate alclad two sides, over 0.187 to 1.000 inch (over 4.750 to 25.40 mm) in nominal thickness, supplied in the -T3/-T351 temper.
Aluminum Alloy, Drawn, Round Seamless Tubing 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti - (2219-T8511) Solution Heat Treated, Stress Relieved by Stretching and Precipitation Heat Treated
This tubing has been used typically for structures requiring good fusion weldability and a combination of good strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.
Aluminum Alloy, Alclad Sheet and Plate, 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti, Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked, Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved
This specification covers an aluminum alloy in the form of alclad sheet and plate 0.020 to 0.499 inch (0.51 to 12.67 mm) inclusive, in nominal thickness (see 8.4).
Aluminum Alloy, Clad One Side, Sheet, 1.25 Mn - 0.12Cu (No. 11-0 Brazing Sheet), Annealed
Castings, Aluminum Alloy Sand, 5.0Si - 1.2Cu - 0.50Mg (355.0-T71), Solution Heat Treated and Overaged
Forgings, Magnesium Alloy, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated
Magnesium Alloy Castings, Sand 6.0Al - 3.0Zn (AZ63-T6) Solution and Precipitation Heat Treated
Magnesium Alloy Castings, Sand 8.7Al - 0.70Zn (AZ91C-T6) Solution Heat Treated and Aged
Aluminum Alloy, Hand Forgings, 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr (7085-T7452), Solution Heat Treated, Compression Stress-Relieved, and Overaged
Aluminum Alloy, Alclad Sheet 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-0) Annealed, Fine Grained
This sheet has been used typically for severely formed structural parts which will be subsequently heat treated and painted or otherwise protected from corrosion, but usage is not limited to such applications.
Certain design and processing procedures may cause this sheet to become susceptible to stress-corrosion cracking after heat treatment; SAE ARP 823 recommends practices to minimize such conditions.
Aluminum Alloy, Extrusion, 2.7 Cu - 1.8 Li - 0.7 Zn - 0.3 Mn - 0.3 Mg - 0.08 Zr (2099-T83), Solution Heat Treated, Stress Relieved by Stretching 1% to 4% and Aged
Aluminum Alloy Extrusions 7.9Zn - 1.6Cu - 2.2Mg - 0.16Cr (7249-T76511) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged
These extrusions have been used typically for structural applications requiring a combination of high tensile strength and good corrosion resistance where intergranular attack is unacceptable, but usage is not limited to such applications.