GTS Mod 6 Easy
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Questions and Answers

What is the duty cycle of the ignition system mentioned in the text?

  • 1 minute on and 4 minutes off
  • 2 minutes on and 3 minutes off (correct)
  • 3 minutes on and 2 minutes off
  • 5 minutes on and 5 minutes off

What is the purpose of selecting full ignition to both or either igniter plug with a continuous duty cycle ignition system?

  • To reduce fuel consumption during harsh weather conditions.
  • To increase the power output of the gas turbine engine.
  • To provide continuous engine relight capability during aircraft takeoff or landing. (correct)
  • To improve the speed-sensitive control of the engine.

Which component de-energizes the ignition relay above 65% RPM according to the text?

  • Paralleling valve
  • Igniter plugs
  • Manifold drain valve
  • HEIU (correct)

When would aircrew typically select just one igniter plug in a gas turbine engine system?

<p>During cruise flight when delayed engine relight is not critical. (B)</p> Signup and view all the answers

What type of ignition system do gas turbine engines typically have?

<p>Dual high energy ignition system (B)</p> Signup and view all the answers

What does the high tension ignition harness supply voltage to?

<p>HEIUs (A)</p> Signup and view all the answers

In the context of the text, what is the purpose of the igniter plugs?

<p>To ignite the air-fuel mixture (C)</p> Signup and view all the answers

Which components are part of a typical ignition system according to the text?

<p>AC or DC bus ignition circuit breaker, high energy ignition unit, ignition relay (A)</p> Signup and view all the answers

What differentiates AC and DC igniter systems in gas turbine engines?

<p>The operating voltages of the systems (C)</p> Signup and view all the answers

What happens when the ignition system is de-energized by the above 65% switch?

<p>The HEIU is de-energized (B)</p> Signup and view all the answers

Why would aircrew select full ignition capability during aircraft takeoff or landing?

<p>To ensure continuous engine relight capability in critical situations. (A)</p> Signup and view all the answers

Which part of the gas turbine engine system connects HEIUs to the igniter plugs?

<p>High tension ignition leads (B)</p> Signup and view all the answers

Where does a low tension current ignition system receive power from?

<p>Battery bus (C)</p> Signup and view all the answers

What happens when the energy in a High Energy Ignition Unit (HEIU) reaches a predetermined value?

<p>It dissipates as high-voltage discharge (C)</p> Signup and view all the answers

In a gas turbine engine, what varies between engine designs in terms of ignition systems?

<p>Ignition plug types and their position (D)</p> Signup and view all the answers

From where do high tension current ignition systems receive their power?

<p>Aircraft AC bus (D)</p> Signup and view all the answers

What does the term 'duty cycle' refer to in an ignition system?

<p>The time limit on the operation to prevent component damage (C)</p> Signup and view all the answers

Which bus is used as a power source for the ignition system according to the text?

<p>Battery bus and Aircraft AC bus (B)</p> Signup and view all the answers
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