CH31929-5 TURBINE ENGINE IGNITER

SPECIFICATIONS

• Suitable for Use With: PW308A Series Aircraft Engine
• Domestic/Import: Domestic

FEATURES
• Silver-plated shell for protection against corrosion and seizing at mechanical interfaces
• Advanced glass and mechanical sealing features design outside the combustor case for protection against gas leakage under high temperature conditions
• Internal configuration designs that optimize heat flow away from terminations to protection sensitive ignition lead components
• Internal termination protective coating to prevent lead component seizing
• Firing end design configurations that can deliver igniter life up to 5000 flight cycles in select applications
• Use of external wear and thermal barrier coatings to protect the life limiting features from wear and thermal distress
• Option for three different semiconductor bodies for low voltage application requirements

TECHNICAL INFORMATION
• FAA-PMA Approved

APPLICATIONS
• Airline
• Business Aviation
• General Aviation
• Space and Military Aircraft Applications