SYSTEM AND METHOD FOR REMOVABLY INSERTING A SENSOR ASSEMBLY INTO A COMPRESSOR CASING

A measurement system (13) for a gas turbine engine (11) is provided. The measurement system (13) comprises a sensor assembly (48). The measurement system (13) also includes multiple sensors (64) coupled to the sensor assembly (48). The sensor assembly (48) is configured to be removably inserted within a space defined by a circumferential track (44, 52, 54) embedded within an inner diameter of a compressor casing (42) of the gas turbine engine (11) without having to disassemble the compressor casing (42).