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Engine : Gas Turbines - 503/277
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You are conducting a borescope inspection of the combustor section of a GE LM2500 gas turbine engine. You observe a one square inch hole in the combustor dome where burn through has removed the metal. What would be your course of action?
A) Record the damage and continue to operate the engine while monitoring the high pressure turbine temperatures and nozzle condition.
B) Immediately take the engine out of service.
C) Operate the engine only in an emergency and at reduced load.
D) Make temporary repairs with on board repair kit to patch hole.
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