GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION

A gas turbine engine (20) includes a compressor (24), a combustor (56) fluidly connected to the compressor (24) via a primary flowpath (C), a turbine (28) fluidly connected to the combustor (56) via the primary flowpath (C), an engine controller (160) communicatively coupled to at least one sensor (70) in the gas turbine engine (20), the controller (160) including a non-transitory memory and a processor, and the at least one sensor (70) including an inlet temperature and/or pressure sensor, wherein the sensor (70) is disposed aft of a fan (130).