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T-34C AIRCRAFT SYSTEMS FAMILIARIZATION WORKBOOK
CHAPTER TWO
STUDY QUESTIONS
1.
The T-34C aircraft is powered by a _______________ engine and its air flow is
____________-____________ type. Maximum shaft horsepower is ________ SHP, ________
ft-lbs. torque; NATOPS (normal) operation is limited to ________ SHP, ________ ft-lbs.
2.
The primary purpose of the engine is to rotate the _______________ through the
______________ gearbox.
3.
The compressor inlet case directs ____________ ____________ to the compressor.
4.
The engine has a ________:________ compression ratio and uses a three-stage
____________compressor and a ________ stage centrifugal compressor.
5.
Two air sources are derived from tapoffs on the diffuser: ____________ and
___________.
6.
The combustion chamber is an ____________, ____________-____________ type.
Combustion results from fuel injected by ________ fuel nozzles and ignited by ________ igniter
plugs.
7.
Once the engine is started, there is no further need to continue ignition with the igniters;
i.e., the engine combustion is self-sustaining. ____________(True/False)
8.
The compressor turbine is also called the ________ turbine and has a maximum rotation
speed of________ RPM which is rated at ________% N1.
9.
The power turbine is also called the ____________ turbine and has a maximum rotation
speed of____________ RPM.
BASIC ENGINE CONSTRUCTION
2-5


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