Engine Air System Flashcards

(14 cards)

1
Q

What percentage of the primary airflow is mixed with fuel and combusted?

A

20% to 25%

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2
Q

Which component/area is supplied with air when the inducer vent operates above approximately 97.5% NG?

A

Low Pressure (LP) compressor

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3
Q

When the NG is below approximately 97.5% the inducer vent relieves which area of the engine of excess pressure?

A

1st stage Low Pressure (LP) compressor

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4
Q

Within the engine air system what condition is the Acceleration Bleed Valve (ABV) in when it “fails safe”?

A

De-energised closed (acceleration control lost ECU is degraded)

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5
Q

How is anti-icing achieved on the aircraft’s engine intake fairings?

A

By electrothermally heated matting

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6
Q

With electrical power ON, what is the state of the engine’s anti-ice air bleed valve solenoid and the valve when the engine anti-icing system is selected to OFF?

A

Solenoid energised, anti-icing valve closed

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7
Q

Where are the engine anti-icing ON/OFF push button indicators located?

A

On the right side of the overhead console

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8
Q

What is the location of the anti-ice test switch?

A

Panel KG, right side of the interseat console below right hand collective lever

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9
Q

The Ice Protection Control Unit’s (IPCU) Continuous Built-In Test (CBIT) has generated a [DE-ICE2 FAIL] caution on the Warnings, Cautions and Advisories (WCA) window. What does this signify?

A

The CBIT has detected a fault in the oil cooler inlet de-ice zones - No. 2 engine intake anti-icing system is unaffected

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10
Q

What does the Integrated Display Unit (IDU) Warnings, Cautions and Advisories (WCA) green advisory alert [ANTI-ICE1] signify?

A

The No. 1 intake anti-icing system is switched on and the anti-ice air bleed valve open

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11
Q

Which type of engine air is used for engine anti-icing purposes?

A

P2.5 air and/or P3.0 air

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12
Q

Which condition will initiate an [ENG# A/ICE] caution on the Warnings, Cautions and Advisories (WCA) area of the Integrated Display Unit (IDU)?

A

A difference between the anti-ice switch selection and the expected feedback from the anti-ice port pressure switch

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13
Q

What is the normal operating temperature range of the electrically heated engine intake mats?

A

65 °C to 140 °C

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14
Q

Within the engine intake anti-icing system how is a critical failure indicated within the cockpit?

A

A [INTAKE# A/ICE] Warnings, Cautions and Advisories (WCA) caution, a green ON and yellow FAIL on the engine anti-ice push button indicator

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