TDS PDF

St SAE AMS-C-7438A-2014

Core Material, Aluminum, for Sandwich Construction. Original standard SAE AMS-C-7438A-2014 in PDF full version. Additional info + preview on request

Document status: Active

€35
St SAE AMS-C-8073-2013

Core Material, Plastic Honeycomb, Laminated Glass Fabric Base for Aircraft Structural and Electronic Applications. Original standard SAE AMS-C-8073-2013 in PDF full version. Additional info + preview on request

Document status: Active

€35
St SAE AMS-C-8837-2008

Coating, Cadmium (Vacuum Deposited). Original standard SAE AMS-C-8837-2008 in PDF full version. Additional info + preview on request

Document status: Replaced by St SAE AMS-C-8837A-2015

€35
St SAE AMS-C-9084-2013

Cloth, Glass, Finished, For Resin Laminates. Original standard SAE AMS-C-9084-2013 in PDF full version. Additional info + preview on request

Document status: Active

€35
St SAE AMS-C-19853-1998

Carbon Removing Compound (For Use in Agitated Tank). Original standard SAE AMS-C-19853-1998 in PDF full version. Additional info + preview on request

Document status: Replaced by St SAE AMS-C-19853A-2021

€35
St SAE AMS-C-27725C-2008

Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C). Original standard SAE AMS-C-27725C-2008 in PDF full version. Additional info + preview on request

Document status: Replaced by St SAE AMS-C-27725E-2025

€35