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SAE J 1939/11:2016-12-06 Physical Layer, 250 Kbps, Twisted Shielded Pair
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 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 ARP 1821B:2016-12-01 Aircraft Ground Flotation Analysis Methods
SAE ARP 5369B:2016-12-01 Guidelines for Wire Identification Marking Using the Hot Stamp Process (Stabilized: Dec 2016)
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