TDS PDF

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

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

Coatings, Cadmium, Tin-Cadmium and Zinc (Mechanically Deposited). Original standard SAE AMS-C-81562-2011 in PDF full version. Additional info + preview on request

Document status: Replaced by St SAE AMS-C-81562A-2018

Core Material, Plastic Honeycomb, Nylon Paper Base for Aircraft Structural Applications. Original standard SAE AMS-C-81986-1998 in PDF full version. Additional info + preview on request

Document status: Active

SHIM STOCK, LAMINATED, BRASS. Original standard SAE AMS-DTL-22499-2a-2011 in PDF full version. Additional info + preview on request

Document status: Replaced by St SAE AMS-DTL-22499-2B-2017

Insulation Sleeving, Electrical, Heat Shrinkable, Crosslinked Chlorinated Polyolefin, Flexible. Original standard SAE AMS-DTL-23053-1A-2012 in PDF full version. Additional info + preview on request

Document status: Replaced by St SAE AMS-DTL-23053-1B-2018