Champion Aviation® Turbine Engine Igniter CH34055

Champion CH34055 Turbine Engine Igniter provides high spark energy to ignite the air fuel mixture in the combustion chamber. To withstand harsh combustor conditions, the turbine engine igniter CH34055 design makes optimal use of super alloys, coatings, air-cooled tip designs and high temperature sealing characteristics. This igniter is designed with fuel drain slots that prevent the igniter from quenching. CH34055 Igniter offers high-performance, extended installed life despite the harsh environmental conditions in the combustion chamber.

FEATURES
• Internal termination protective coating to prevent lead component seizing
• Excellent resistance to wear
• Corrosion resistance

BENEFITS
• Optimize heat flow away from terminations to protection sensitive ignition lead components
• Highly reliable in harsh environmental conditions

NOTE
Alternates with 3035102. Interchangeable with CH34406, CH34511, 3900274, 3900275, 3035882, 3035102, 10-390667-1, 3031213 and NSN 2305-01-052-0636 on PT6, ST6l-73 AND PW901Aapplications. Always check application charts for correct part numbers.