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DESCRIPTION
Champion Aerospace Turbine Engine Igniter
Silver-plated shell for protection against corrosion and seizing at mechanical interfaces
Advanced glass and mechanical sealing feature design outside the combustor case for protection against gas leakage under high temperature conditions.
Internal configuration design that optimizes heat flow away from terminations to protect sensitive ignition lead components
Internal termination protective coating to prevent lead component seizing
Use of external wear and thermal barrier coatings to protect the life limiting features from wear and thermal distress