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SAE AS 4914D:2016-12-13 Aircraft...
SAE AMS 4909K:2016-12-06 Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn, Extra Low Interstitial Annealed
SAE AMS 4962B:2016-12-06 Titanium Alloy, Investment Castings 6Al - 4V Hot Isostatically Pressed (Stabilized: Dec 2016)
SAE AMS 3970/1A:2016-12-06 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements
SAE AMS 3970/2A:2016-12-06 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg
SAE AMS 3970/3A:2016-12-06 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Carbon Prepreg
SAE AMS 3970/4A:2016-12-06 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive
SAE AMS 3970A:2016-12-06 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction
SAE J 2601:2016-12-06 Fueling Protocols for Light Duty Gaseous Hydrogen Surface Vehicles
SAE AS 6286/6:2016-12-05 Deicing/Anti-Icing Diagrams/No Spray Zones
SAE AMS 3970/5:2016-12-05 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 5 - Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg
SAE AMS 3970/6:2016-12-05 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 6 - Material Specification: Carbon Fiber Fabric Reinforced Epoxy Prepreg for Repair, Plain Weave Fabric, 193 g/m2, Adhesive Film for Repair and Non-Structural Glass Fiber Fabric Reinforced Epoxy Prepreg, 105 g/m2
SAE J 1939/14:2016-12-01 Physical Layer, 500 Kbps