Study Questions -Cont. - P-307

T-34C AIRCRAFT SYSTEMS FAMILIARIZATION

CHAPTER EIGHT

WORKBOOK

14. Select the correct statement(s) pertaining to the fuel topping function(s) by circling the

correct letters.

Bleeds HP oil from prop shaft if propeller RPM reaches 2332

Increases blade angle to slow propeller RPM

Bleeds Py air causing fuel flow decrease in order to protect the power turbine

Bleeds P3 air in the event of an overtorque condition

15.

Correctly complete the following statement.

The torque limiter is mounted on the ____________ gearbox and is used to limit engine output

power to ____________ by bleeding ____________ air.

16.

Write the location and purpose of the EPL.

POWER PLANT CONTROL SYSTEM 8-9