PC12 NGX Engine Quiz Copy Copy

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Question 1 of 11

1. Question
What is the correct statement regarding the engine?
- The engine parameters are EGT, NF and N2.
- The engine shaft is directly connected between the compressor unit and the propeller
- Its a heavy duty turbo fan engine
- Free turbine, reverse flow engine
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Question 2 of 11

2. Question
How can the pilot prevent FOD from entering the engine?
- By open the Inertial Separator
- By closing the Inertial Separator
- By adjusting the pitch to fine pitch
- Not to land on contaminated surfaces
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Question 3 of 11

3. Question
What is controlling the engine power?
- The EPECS
- The PCL with direct link to the FCU
- The EEC
- The MAU
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Question 4 of 11

4. Question
What is the purpose of the Purge Air?
- To create a motive flow pressure for the return line.
- The rise the pressure in the purge line and fuel nozzles
- To pressurize the motive flow line
- To purge the fuel nozzles from any unused fuel during engine shutdown
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Question 5 of 11

5. Question
What is the correct statement?
- The Fuel/oil heat exchanger is located after the Engine driven High Pressure fuel pump but before the low pressure pump.
- Fuel is pre heated before it reaches the Engine driven Low pressure fuel pump
- Fuel is pre heated before it reaches the Engine driven High pressure fuel pump
- The Fuel filter is located before the Fuel / Oil heat exchanger
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Question 6 of 11

6. Question
The ODM, Oil Debris Monitoring measures what?
- Particles over 30s and 120s periods
- temperature in the engine oil system
- Particles in the oil line, based on size only
- Magnetic chip detector system in the engine oil reservoir
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Question 7 of 11

7. Question
What is the Torque limit at Sea Level?
- 67 psi
- 104%
- 44.84 psi
- 46.1 psi
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Question 8 of 11

8. Question
What is a true statement?
- The EPECS does not limit power in order to prevent exceedance of engine parameters in flight.
- The EPECS will limit the power in order to prevent exceedance of engine parameters in flight.
- The EPECS is a single channel, dual processor full authority integrated engine and propeller control system.
- The EPECS prevent the engine to transition into the reverse range in flight if the PCL is intentionally lifted and moved into the reverse range.
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Question 9 of 11

9. Question
During engine start, when does the Ignition turns off if in AUTO?
- When the condition lever is set to ground idle
- When the NG is above 50%
- after 10 seconds after the ITT is above 500 C
- above 50% NG
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Question 10 of 11

10. Question
What is the correct statement?
- Engine compartment has a Fire Detection system made of visual smoke detectors.
- The Engine Compartment has one two Fire Detection loops and One Fire Extinguisher Bottle
- The engine has a Fire Detection system only, if fault detected it will only show on landing as advisory in the CAS
- The engine has a Fire Detection system only.
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Question 11 of 11

11. Question
What are the limitations for engine start between each engine start attempt?
- 120 sec off, 120 sec off, 30 min off
- 60 sec off, 60 sec off, 60 min off
- 60 sec off, 120 sec off, 30 min off
- 60 sec off, 60 sec off, 30 min off
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PC12 NGX Engine Quiz Copy Copy

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