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CHAPTER EIGHT
T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
WORKBOOK
ANSWERS TO STUDY QUESTIONS
1.
power output, speed, condition, left
2.
2, 3
1, 4
3.
Power and beta
4.
Fuel off, feather, RPM
5.
reduction
6.
a., c.
7.
6, 2
3, 5
1, 4
8.
overspeed, high pressure oil, reduction gearbox, increase
9.
b., c.
10.  It is located on the reduction gearbox; it limits propeller RPM should the primary propeller
governor fail.
11. 2332; higher
12.
1950, 2150, 400, 500
13.  To control power turbine overspeed should there be a failure or malfunction of the
propeller pitch change assembly.
14.
c.
reduction, 550 SHP (1315 ft-lbs.), Py air
15.
16.  On the power control quadrant, the EPL provides a direct mechanical linkage to the
bellows and metering pin in the FCU.
8-10 POWER PLANT CONTROL SYSTEM


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