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CHAPTER FOUR
T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
WORKBOOK
STUDY QUESTIONS
1.
Primary fuel for the T-34C is ____________ and alternates are ____________
or____________.
2.
The total fuel capacity is ____________ ____________ of which ____________
____________ are usable.
3.
The fuel quantity indicators provide fuel quantity in gallons. ____________(True/False)
4.
Illumination of either FUEL LOW indicator indicates approximately ____________
____________ of usable fuel in that respective tank/wing.
5.  Illumination of a steady yellow FUEL PRESS light indicates possible failure of the
____________ driven ____________ ____________ pump. Activate the ____________
standby ____________ pump by turning on the switch in the ____________ cockpit.
6.
If the Fuel Shutoff "T" handle in the front cockpit is pulled while the aircraft is on the
ground, you may reset the "T" handle. ____________(True/False)
7.
The engine-driven fuel boost pump is mounted to and driven by the ____________ oil
____________ ____________.
8.
If the primary fuel pump fails, the engine continues to run. ____________(True/False)
9.
The fuel scavenge pump is mounted on the ____________ side of the firewall.
10.  With illumination of the green ignition light a false increase will be seen on the
______________________ indicator due to spurious input from the excitor.
4-8 FUEL SYSTEM


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