021.06 PNEUMATICS - PRESSURISATION AND AIR-CONDITIONING SYSTEMS Flashcards

1
Q

On modern large pressurised jet transport aeroplanes, the maximum cabin differential pressure is approximately (…) ​psi.

A

On modern large pressurised jet transport aeroplanes, the maximum cabin differential pressure is approximately (7-9) psi.

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2
Q

The bleed air gauge measures air pressure relative to (cabin/atmospheric/total)​ pressure.

A

The bleed air gauge measures air pressure relative to (atmospheric) pressure.

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3
Q

The excess cabin altitude alerting system must operate to warn the crew at (…) ​ft.

A

The excess cabin altitude alerting system must operate to warn the crew at (10 000) ft.

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4
Q

Cabin air for modern transport airplanes is usually taken from the (low/high) pressure stage of the (LP/HP) compressor and from the (low/high) pressure stage of the (LP/HP)​ compressor if necessary.

A

Cabin air for modern transport airplanes is usually taken from the (low) pressure stage of the (HP) compressor and from the (high) pressure stage of the (HP) compressor if necessary.

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5
Q

Name the two modes of operation used in most cabin pressurization systems and in which phase of flight it’s used.

A

Name the two modes of operation used in most cabin pressurization systems and in which phase of flight it’s used.

  • isobaric mode → during cruise
  • constant pressure differential mode → during climb/descent
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6
Q

In a large transport aeroplane the main temperature reduction of the conditioned air is achieved in the (heat exchangers/expansion turbine/evaporator/condenser)​.

A

In a large transport aeroplane the main temperature reduction of the conditioned air is achieved in the (heat exchangers).

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7
Q

In the pneumatic supply system of a modern transport aircraft, the air pressure is regulated. This pressure regulation occurs just before the manifold by the (high pressure bleed air/low pressure bleed air/intermediate pressure check/fan bleed air)​ valve.

A

In the pneumatic supply system of a modern transport aircraft, the air pressure is regulated. This pressure regulation occurs just before the manifold by the (low pressure bleed air) valve.

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8
Q

Consider a piston engined aircraft. Pneumatic air is taken from (ram air/supercharger air/inlet air manifold)​.

A

Consider a piston engined aircraft. Pneumatic air is taken from (supercharger air).

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9
Q

If the maximum certified altitude of an aeroplane is limited by the pressurised cabin, this limitation is due to the maximum (positive/negative)​ cabin differential pressure at maximum cabin altitude.

A

If the maximum certified altitude of an aeroplane is limited by the pressurised cabin, this limitation is due to the maximum (positive) cabin differential pressure at maximum cabin altitude.

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10
Q

Under normal conditions (EASA CS-25) the cabin pressure altitude of a transport aeroplane is not allowed to exceed (…)​ ft.

A

Under normal conditions (EASA CS-25) the cabin pressure altitude of a transport aeroplane is not allowed to exceed (8000) ft.

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