T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
Write the purpose of the interstage turbine temperature sensing system.
Normal ITT operating range is ____________ to ____________ and maximum continuous
temperature is ____________.
There are ____________ thermocouples providing inputs to the ITT indicators.
Idle RPM on the turbine tachometer (N1) is ____________ to ____________.
The N1 turbine tachometer receives its input from the ____________ - ____________
mounted on the____________ gearbox.
High temperature in the engine compartment will be sensed by the three infrared detectors
and cause the "FIRE" light to illuminate. ____________ (True/False)
The engine fire detection system is a ____________ ____________ system that provides a
____________ warning of a(n) ____________ compartment fire.
The fire warning light will _______________ when a fire is no longer present.
The ITT indication is internal to the engine, while the fire warning light relates to what
ENGINE INSTRUMENTATION AND FIRE DETECTION SYSTEMS