NA 131
DIN Standards Committee Aerospace
DIN EN 7010 [CURRENT] references following documents:
| Document number | Edition | Title |
|---|---|---|
| SAE AMS 5845K | 2019-07-24 | Alloy, Corrosion-Resistant, Round Bars, 20Cr - 35Ni - 35Co - 10Mo, Vacuum Induction Plus Consumable Electrode Vacuum Remelted, Solution Heat Treated, Work Strengthened, and Aged More |
| SAE AMS 5937A | 2018-11-02 | Steel, Corrosion-Resistant, Bars, Wire, and Forgings, 12Cr - 11Ni - 2Mo - 1.5Al - 0.3Ti, Vacuum Induction Plus Vacuum Consumable Electrode Melted, Solution Heat Treated, Precipitation Hardenable More |
| SAE AMS 6325L | 2020-04-10 | Steel, Bars, and Forgings, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740), Heat Treated, 105 ksi (724 MPa) Tensile Strength More |
| SAE AMS 6947B | 2019-01-07 | Titanium Alloy, Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, Annealed, Heat Treatable More |
| SAE AMS-QQ-S-763D | 2015-03-02 | Steel, Corrosion Resistant, Bars, Wire, Shapes, and Forgings More |
| SAE AMS-S-6758B | 2017-11-30 | Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) More |
| SAE AS 8879D | 2004-08-09 | Screw Threads - UNJ Profile, Inch Controlled Radius Root with Increased Minor Diameter More |
| WL 1.4534-1 | 2012-10 | Aerospace series - High-strength precipitation-hardening stainless chromium-nickel-molybdenum-aluminium steel with approx. 0,04 C - 13 Cr - 8 Ni - 2,2 Mo - 1 Al - Part 1: Bars and forgings More |
| WL 1.4944-3 | 1984-07 | High temperature precipitation-hardening nickel-chromium-titanium steel with about 0.06C-25Ni-15Cr-2.1Ti-1.2Mo; rods and wire for screws and nuts More |
| WL 1.6604-1 | 1982-03 | Heat-treatable chromium-nickel-molybdenum steel with about 0.3C-2Cr-2Ni-0.4Mo; rods and forgings More |
