General Agreement Related to Use of 5D Elongations in the SI tensile property tables
Aluminum Alloy, Plate, 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T34), Solution Heat Treated and Stress Relieved
This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 6.500 inches (12.70 to 165.00 mm) in nominal thickness (see 8.5).
Aluminum Alloy, Extruded Wide Panel Profiles (7150-T77511) 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr Solution Heat Treated, Stress-Relieved, Straightened and Overaged
Aluminum Alloy, Extruded Rod, Bar, and Profiles (7055-T76511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and Overaged
Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged
This specification covers an aluminum alloy in the form of plate.
Aluminum Alloy, Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated
Aluminum Alloy, Plate (7160-T7351) 7.0Zn – 2.2Cu – 1.5Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and Overaged
Aluminum Alloy Tubing, Seamless, Drawn 4.4Cu - 1.5Mg - 0.60Mn (2024-O) Annealed
Aluminum Alloy, Extrusion 2.7Cu - 1.8Li - 0.7Zn - 0.3Mn - 0.3Mg - 0.08Zr (2099-T83) Solution Heat Treated, Stress Relieved by Stretching 1 to 4% and Aged
Aluminum, Foil and Light Gage Sheet, 99.45Al (1145-0) Annealed
Aluminum Alloy, Seamless Drawn Tubing 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T4) Solution Heat Treated and Naturally Aged
Aluminum Bronze Bars, Rods, and Forgings, 90.5Cu - 7.5Al - 1.9Si, Stress Relieved
Copper-Nickel-Tin Alloy Castings, Cu – 15Ni – 8Sn, Hot Isostatically Pressed, Solution Annealed and Spinodal Heat Treated
Test Method and Limits for Bow Height of Aluminum Sheet Samples After Chemical Milling
This specification covers requirements for testing wrought aluminum alloy raw material in the form of sheet by producers.
This Aerospace Standard applies only to heat treated, flat sheet in the heat treated condition (T3X, T6X, T7X, or T8X) temper, and having thicknesses in the range 0.032 to 0.249 inch (0.8 to 6.3 mm). Purchasers are encouraged to contact producers with questions on the availability of material (i.e. alloy/temper/width) that is capable of meeting the requirements of this standard. Product having the capability prescribed by this specification is available in limited quantities and tempers because of the special processing required. NOTE: Sheet in the coiled form cannot be supplied to this specification.