SAE AMSC81986 Core Material, Plastic Honeycomb, Nylon Paper Base for Aircraft Structural Applications standard by SAE International, 08/10/2022
SAE AMSC8073 Core Material, Plastic Honeycomb, Laminated Glass Fabric Base for Aircraft Structural and Electronic Applications standard by SAE International, 08/10/2022
SAE AMS3715D Core, Honeycomb, Glass/Phenolic standard by SAE International, 08/10/2022
SAE AMS3109 Primer, Adhesive, Electrodeposited -55 to +82 °C (-67 to +180 °F) standard by SAE International, 08/10/2022
SAE AMS3107/4A Primer, Adhesive, Corrosion-Inhibiting High Durability Epoxy, -55 to +215 °C (-67 to +419 °F) standard by SAE International, 08/10/2022
SAE AMS3913B Radome, Foam Sandwich Hot-Melt, Addition-Type Polyimide standard by SAE International, 08/10/2022
SAE ARP6539 Validation and Verification Process Steps for Monitors Development in Complex Flight Control and Related Systems standard by SAE International, 08/10/2022
SAE AMS3714D Core, Overexpanded Honeycomb, Polyamide Paper Base, Phenolic Coated standard by SAE International, 08/10/2022
SAE AMS3688B Adhesive, Foaming, Honeycomb Core Splice, Structural −55 to +82 °C (−65 to +180 °F) standard by SAE International, 08/10/2022
SAE AMS3689B Adhesive, Foaming, Honeycomb, Core Splice, Structural −54 to +177 °C (−65 to +350 °F) standard by SAE International, 08/10/2022
SAE AMS3107/1A Primer, Adhesive, Corrosion-Inhibiting High Durability Epoxy, -55 to +95 °C (-67 to +203 °F) standard by SAE International, 08/10/2022
SAE AMS3716C Core, Honeycomb, Glass/Phenolic Bias Weave Fiber Construction standard by SAE International, 08/10/2022