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|  CHAPTER SEVEN
T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
WORKBOOK
ANSWERS TO STUDY QUESTIONS
1.
Constant, hydraulically, full-feathering, reversible
2.
b., d., e., g.
3.
The angle between the plane of rotation of the propeller and the chord line of the blade
4.
1.
feather
2.
idle low pitch stop
3.
beta
5.
Spring, connecting links, counterweights
6.
b., d.
7.
Reverse, negative
8.
a., d.
9.
DC power available to operate the solenoid
The nose landing gear strut compressed
The BETA switch on top of the PCL depressed
10. In RPM range:
7-8 PROPELLER
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