SAE AMS-S-83318B-2011 PDF

Scope: This specification covers two-component polysulfide sealing compounds, temperature resistant, for use from -65 to 250 °F (-54 to 121 °C), low temperature curing from 20 °F (-13 °C) minimum, for quick repair of integral fuel tanks and fuel cell cavities. During application, sealing compound shall exhibit suitable, fluid consistency.

SAE AMS-S-83318B-2011 Referenced Document

SAE AMS-C-27725-1999 Coating@ Corrosion Preventative@ Polyurethane for Aircraft Integral Fuel Tanks for Use to 250 Degrees F (121 Degrees C) (FSC 8030)
SAE AMS-S-8802-1999 Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion
SAE AMS2471 ANODIC TREATMENT FOR ALUMINUM BASE ALLOYS Sulfuric Acid Process
SAE AMS2629 JET REFERENCE FLUID
SAE AMS3100 ADHESION PROMOTER For Polysulfide Sealing Compounds
SAE AMS4045 ALUMINUM ALLOT SHEET AND PLATE 5.6Zn - 2.5Mg - 1.6Cu - 0.25Cr (75S-T6)
SAE AMS4911 TITANIUM ALLOY SHEET 6Al – 4V Annealed – 120@000 psi Yield
SAE AS5127-1997 Methods for Testing Aerospace Sealants
SAE AS5127/1-1997 Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds

2011 SAE AMS-S-83318B-2011 Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities