Day 3 Progress Check Flashcards

1
Q

How are most turbine ignition systems cooled?

A

Air cooling

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2
Q

What condition(s) may cause the engine to flame out in-flight, requiring to relight?

A

Foreign object ingestion

Severe precipitation

Flight above certain altitudes

Correct: All of the above

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3
Q

What should be examined for flashover and carbon tracking?

A

Grommet seal

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4
Q

What is the difference between turbine engine ignition systems and reciprocating engine ignition systems?

A

Turbine systems may use continuous ignition

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5
Q

What is the purpose of dual igniters in turbine ignition systems?

A

Improved safety through redundancy

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6
Q

What is the potential danger associated with the high energy level and voltage of turbine ignition systems?

A

Injury or death if carelessly handled during maintenance

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7
Q

What is the significance of a larger electrode gap in the igniter plug compared to a spark plug?

A

It allows for easier spark arcing

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8
Q

What caution should be emphasized when checking the igniter?

A

Personnel safety due to high energy and voltage

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9
Q

What type of electrical energy is used by the igniter plug to create the spark?

A

High-voltage DC

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10
Q

In which flight condition is continuous ignition typically used in turbine engines?

A

Takeoff, landing, and emergencies

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11
Q

What is the primary purpose of continuous ignition in turbine engines during critical flight modes?

A

Preventing engine flameout

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12
Q

What is the purpose of the annular-gap igniter plug in a turbine engine?

A

Projecting into the combustion chamber for a more effective spark

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13
Q

How is the igniter checked by maintenance personnel listening for a clicking noise?

A

During engine start

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14
Q

What differentiates the annular-gap igniter plug from the constrained-gap plug?

A

Projecting into the combustion chamber

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15
Q

What is the role of the high-energy ignition unit?

A

Transforming and stepping up power for igniters

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