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CHAPTER FIVE
T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
WORKBOOK
STUDY QUESTIONS
1.
Write the purpose of the interstage turbine temperature sensing system.
2.
Normal ITT operating range is ____________ to ____________ and maximum continuous
temperature is ____________.
3.
There are ____________ thermocouples providing inputs to the ITT indicators.
4.
Idle RPM on the turbine tachometer (N1) is ____________ to ____________.
5.
The N1 turbine tachometer receives its input from the ____________ - ____________
mounted on the____________ gearbox.
6.
High temperature in the engine compartment will be sensed by the three infrared detectors
and cause the "FIRE" light to illuminate. ____________ (True/False)
7.
The engine fire detection system is a ____________ ____________ system that provides a
____________ warning of a(n) ____________ compartment fire.
8.
The fire warning light will _______________ when a fire is no longer present.
9.
The ITT indication is internal to the engine, while the fire warning light relates to what
area?
5-4
ENGINE INSTRUMENTATION AND FIRE DETECTION SYSTEMS


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