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BS PD CEN ISO/TR 20659‑2:2024 Rheological test methods. Fundamentals...

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SAE AMS3107/1APrimer, Adhesive, Corrosion-Inhibiting High Durability Epoxy, -55 to +95 °C (-67 to +203 °F)standard by SAE International, 08/10/2022
SAE AMSC7438ACore Material, Aluminum, for Sandwich Constructionstandard by SAE International, 08/10/2022
SAE AMSC81986Core Material, Plastic Honeycomb, Nylon Paper Base for Aircraft Structural Applicationsstandard by SAE International, 08/10/2022
SAE AMS3913BRadome, Foam Sandwich Hot-Melt, Addition-Type Polyimidestandard by SAE International, 08/10/2022
SAE AMS3714DCore, Overexpanded Honeycomb, Polyamide Paper Base, Phenolic Coatedstandard by SAE International, 08/10/2022
SAE AMS3107/2APrimer, Adhesive, Corrosion-Inhibiting High Durability Epoxy, -55 to +120 °C (-67 to +248 °F)standard by SAE International, 08/10/2022
SAE AMS3712CCore, Honeycomb, Glass/Polyimidestandard by SAE International, 08/10/2022
SAE AMS3715DCore, Honeycomb, Glass/Phenolicstandard by SAE International, 08/10/2022
SAE AMSC8073Core Material, Plastic Honeycomb, Laminated Glass Fabric Base for Aircraft Structural and Electronic Applicationsstandard by SAE International, 08/10/2022
SAE AMS4031KAluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-O) Annealed or, When Specified, “As Fabricated” (2219-F)standard by SAE International, 08/17/2022
SAE AMS4029MAluminum Alloy, Sheet and Plate (2014; -T6 Sheet, -T651 Plate) Solution and Precipitation Heat Treatedstandard by SAE International, 08/17/2022
SAE AMS5662PNickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Stock for Forgings and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenablestandard by SAE...