Turkmenistan standards PDF
Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 5 - Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg. Original standard SAE AMS3970-5-2016 in PDF full version. Additional info + preview on request
Document status: Replaced by St SAE AMS3970-5A-2026
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. Original standard SAE AMS3970-6-2016 in PDF full version. Additional info + preview on request
Document status: Active
Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction. Original standard SAE AMS3970A-2016 in PDF full version. Additional info + preview on request
Document status: Replaced by St SAE AMS 3970B-2026
Aluminum Sheet and Plate (1060-0). Original standard SAE AMS4000F-2014 in PDF full version. Additional info + preview on request
Document status: Active
Aluminum Sheet and Plate, 0.12Cu (1100-0), Annealed. Original standard SAE AMS4001J-2007 in PDF full version. Additional info + preview on request
Document status: Active
Aluminum Alloy Tubing, Seamless, Drawn 1.8Cu - 1.0Mg - 0.8Si - 0.20Cr Solution Heat Treated, Stress-Relieved by Stretching, and Aged (2013-T6511). Original standard SAE AMS4002B-2024 in PDF full version. Additional info + preview on request
Document status: Active