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|  CHAPTER THREE
T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
CHANGE 2
WORKBOOK
ANSWERS TO STUDY QUESTIONS
1.
It allows solid particles to be separated from the inlet air and vented overboard. It is
activated by the front cockpit pilot.
2.
The oil cooler, the starter/generator, the engine-driven accessories, and the cockpit.
3.
In the main oil tank.
4.
It provides additional oil for inverted flight.
5.
The internal pump is inside the accessory gearbox. The external pump is mounted
externally on the accessory gearbox.
6.
Minimum and maximum in hot and cold range and cold range in quart increments.
7.
70 F, 90 F
8.
Oil pressure - right engine support strut; oil temperature - right side of accessory gearbox.
9.
What are the minimum, normal, and maximum limitations for oil temperature and
pressure?
Oil Temperature
Limitations
Oil Pressure
-40 C
Minimum
40 PSI @ idle (62-65% N1)
10 - 99 C
Normal
65 - 85 PSI (above 75% N1)
100 C
Maximum
100 PSI
10.
The starter switch.
11.
12. It provides initial ignition during engine start.
13. It automatically provides a spark for combustion in the event of an engine flameout. It
operates when engine output power drops into the 300 - 180 ft-lbs. range.
3-8 PT6A-25 AIR/OIL/IGNITION SYSTEMS
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