equipped with instrumentation to monitor engine operation during flight measures temperature in the
turbine section.
propeller tachometers (N2) register shaft speed in hundreds of rpm. Each indicator is directly responsive
to a tachometer-generator unit attached to a corresponding engine section.
Oil pressure is taken from the delivery side of the main oil pressure pump and registered in
psi.
Oil temperature is taken from the delivery side of the oil pressure pump and registered in
degrees centigrade.
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