SAE AS7766:2021
Current
Current
The latest, up-to-date edition.
Terms Used in Aerospace Metals Specifications
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
09-15-2021
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.This SAE Aerospace Standard (AS) defines and clarifies terms used in aerospace materials and process specifications, standards, and recommended practices.
| Committee |
AMS B
|
| DocumentType |
Standard
|
| Pages |
11
|
| PublisherName |
SAE International
|
| Status |
Current
|
| SAE AMS2221H | Tolerances Copper and Copper Alloy Bars and Rods |
| SAE AMS4976M:2023 | Titanium Alloy, Forgings 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo - 08Si Solution and Precipitation Heat Treated |
| SAE AMS5629/H1150:2023 | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation Hardened (H1150) |
| SAE AMS2476D | Electrolytic Treatment for Magnesium Alloys Alkaline Type, Full Coat |
| SAE AMS6495C:2022 | Steel Bars, Forgings, Mechanical Tubing, and Forging Stock, 1.0Cr - 2.50Ni - 2.0Mo - 1.10Si (0.10 - 0.20C), Premium Aircraft-Quality, Electroslag Remelted or Consumable Electrode Vacuum Remelted |
| SAE AMS4365A:2022 | Aluminum Alloy, Plate 7.9Zn - 1.2Cu - 2.1Mg - 0.10Zr (7097-T7651) Solution Heat Treated, Stress Relieved, and Overaged |
| SAE AMS4625J:2023 | Phosphor Bronze Bars, Rods, and Tubing 95Cu - 5Sn Hard Temper |
| SAE AMS4374A:2022 | Aluminum Alloy, Extruded Profiles 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged |
| SAE AMS5676G | Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire 80Ni - 20Cr |
| SAE AMS7011:2022 | Electron Beam-Powder Bed Fusion (EB-PBF) Produced Preforms and Parts Titanium Alloy, 6Al - 4V Hot Isostatically Pressed |
| SAE AMS4782H:2022 | Nickel Alloy, Brazing Filler Metal 71Ni - 10Si - 19Cr 1975 °F (1080 °C) Solidus, 2075 °F (1135 °C) Liquidus |
| SAE AMS5784F | Steel, Corrosion- and Heat-Resistant, Welding Wire 29Cr - 9.5Ni |
| SAE AMS5568J | Steel, Corrosion- and Heat-Resistant, Welded Tubing 17Cr - 7.1Ni - 1.1Al Solution Heat Treated, Precipitation-Hardenable |
| SAE AMS2263F | Tolerances Nickel, Nickel Alloy, and Cobalt Alloy Aircraft Tubing |
| SAE AMS6294L:2023 | Steel Bars and Forgings and Forging Stock, Carburizing, Aircraft-Quality 1.8Ni - 0.25Mo (0.17 - 0.22C) (4620) |
| SAE AMS2615G | Pressure Testing, Hydraulic Pressure as Specified |
| SAE AMS6448N | Steel, Bars, Forgings, and Tubing 0.95Cr - 0.22V (0.48 - 0.53C) |
| SAE AMS6427P:2023 | Steel Bars, Forgings, Mechanical Tubing, and Forging Stock, Aircraft Quality, 0.88Cr - 1.8Ni - 0.42Mo - 0.08V (0.28 - 0.33C) (4330 Mod) |
| SAE AMS5680K | Steel, Corrosion- and Heat-Resistant, Welding Wire 18.5Cr - 11Ni - 0.40Cb (Nb) (SAE 30347) |
| SAE AMS4070P:2023 | Aluminum Alloy, Drawn, Round Seamless Tubing 2.5Mg - 0.25Cr (5052-O) Annealed |
| SAE AMS5441C:2023 | Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings Ni - 18Cr - 2.8Mo - 5.5Cb (Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable |
| SAE AMS4895:2023 | Titanium Alloy, Round Bars 5Al - 1Fe Annealed |
| SAE AMS5952:2023 | Nickel Alloy, Corrosion- and Heat-Resistant, Welding and Additive Manufacturing Wire 57Ni - 20Cr - 10Co - 8.5Mo - 2.1Ti - 1.5Al - 0.005B (282) Vacuum Induction Melted and Electroslag or Vacuum Remelted Solution Heat Treated, Cold Worked, Precipitation Heat Treatable |
| SAE AMS4950F:2023 | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Solution Heat Treated and Aged Modified Strength |
| SAE AMS5768M | Alloy, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Rings and Stock for Forgings, Rings and Heading 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N - 31Fe Solution and Precipitation Heat Treated |
| SAE AMS5636H | Steel, Corrosion-Resistant, Bars and Wire 18Cr - 9.0Ni (302) Solution Heat Treated and Cold Drawn 100 ksi (689 MPa) Tensile Strength |
| SAE AMS6272P | Steel Bars, Forgings, and Mechanical Tubing Aircraft-Quality 0.50Cr - 0.55Ni - 0.20Mo (0.15 - 0.20C) (SAE 8617) |
| SAE AMS4964D:2024 | Titanium Alloy Bars, Wire, Forgings, and Rings 4.5Al - 3V - 2Fe - 2Mo Annealed |
| SAE AMS5966D:2024 | Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire 50Ni - 20Cr - 20Co - 5.9Mo - 2.2Ti - 0.45AI (Alloy 263) Consumable Electrode or Vacuum Induction Melted and Remelted |
| SAE AMS5649J | Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, and Stock for Forgings, 18Cr - 13Ni - 2.1Mo (316FM) Free Machining Solution Heat Treated |
| SAE AMS5903D:2024 | Steel, Corrosion-Resistant, Sheet, Strip, and Plate 18Cr - 9.0Ni (302) Cold Rolled, 1/4 Hard, 125 ksi (862 MPa) Tensile Strength |
| SAE AMS5529L:2024 | Steel, Corrosion-Resistant, Sheet and Strip 17Cr - 7.1Ni - 1.1Al (Alloy 17-7) Solution Heat Treated and Cold Rolled, Precipitation Hardenable |
| SAE AMS5800H:2023 | Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire 54Ni - 19Cr - 11Co - 10Mo - 3.2Ti - 1.5Al - 0.006B Vacuum Induction Melted and Remelted |
| SAE AMS6532L:2024 | Steel, Bars and Forgings, and Forging Stock 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C) Vacuum Melted, Normalized and Overaged Precipitation Hardenable |
| SAE AMS3021G:2024 | Fluid, Reference for Testing Di-Ester (Polyol) Resistant Material |
| SAE AMS5801H:2023 | Cobalt Alloy, Corrosion- and Heat-Resistant, Welding Wire 39Co - 22Cr - 22Ni - 14.5W - 0.07La (188) |
| SAE AMS5668L | Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Forging Stock 72Ni - 15.5Cr - 7.0Fe - 2.5Ti - 1.0Cb (Nb) - 0.70Al (X750) 2100 °F (1149 °C) Solution and Precipitation Heat Treated |
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