Gas Turbines USCG Q#496 (Set 8)

Zero reference for the GE LM2500 gas turbine engine is established by the use of which of the following engine components?

Official USCG Answer & Rule Citation

Correct Answer: Option A — Locking lug blades.

Locking lug blades serve as the zero reference point for the GE LM2500 compressor rotor. These specific blades are uniquely identified to establish a baseline for indexing during maintenance, borescope inspections, and blade replacement, ensuring precise alignment and tracking of the rotor assembly throughout the engine's operational life.

Advertisement
All Gas Turbines Sets Practice Set 8