Environmental Control System Flashcards

1
Q
A
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2
Q

What function does the Pneumatic Valve Assembly (PVA) fitted to each engine provide for the Environmental Control System (ECS)?

A

Controls the continuous P3 bleed-air requirement

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3
Q

Where is the Pressure Regulating and Shutoff Valve (PRSOV) located?

A

In the left engine compartment

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4
Q

What is the function of the Pressure Regulating and Shutoff Valve (PRSOV)?

A

To act as an ON/OFF supply valve, regulate engine bleed-air pressure to the Heating and Ventilation System (HVS) and remove pressure variations and surges associated with engine performance

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5
Q

What happens if the HVS fan over heats?

A

The entire heating system latches off, requiring power to be recycled when cool, to reinitiate the system

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6
Q

Where is the Cockpit and Cabin Heating and Ventilation System (CCHVS) fan located?

A

On the left side of the aircraft in the rear bay

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7
Q

How is the Heating and Ventilation System (HVS) fan distribution ducting protected against overpressurisation?

A

The system has two, permanently open, under seat foot vents

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8
Q

Where are the controls for the Heating and Ventilation System (HVS) located?

A

To the left of the Engine Control Panel (ECP) on the overhead console

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9
Q

What is the Environmental Control System (ECS) response if an [HVS DUCT HOT] caution illuminates on the Warnings, Cautions and Advisories (WCA) display?

A

The system is latched off

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10
Q

What is the heating operational response from the Environmental Control System (ECS) after an [HVS DUCT HOT] Warnings, Cautions and Advisories (WCA) indication illuminates, system temperature is not cooling below 90 °C and a reset is attempted?

A

The system will not restart until the temperature reaches a normal limit

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11
Q

When must the Forward Avionic Cooling System (FACS) be operated to maintain a thermal environment?

A

Whenever power supplies are selected “ON”

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12
Q

How is water ingress prevented on the Forward Avionic Cooling System (FACS)?

A

Inlet duct design slows the airstream allowing for water particulates to drop and be expelled via drains on the lower fuselage

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13
Q

Where are the switches for the Forward Avionics Cooling System (FACS) located?

A

On the right side of the overhead console

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14
Q

Assuming both AC and DC power is available if both FACS fans are put to auto what state are the fans in?

A

Primary fan is running and secondary is off.

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15
Q

Why are there two rear bay cooling fans?

A

Redundancy

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16
Q

How may load sharing between the two Rear Bay Cooling System (RBCS) fans be achieved?

A

By manually alternating the fan selection on alternate days to balance operating hours

17
Q

How is a Rear Bay Cooling System (RBCS) [RBCS FAN] caution cleared after a single fan failure without switching the system to OFF?

A

By selecting the alternate RBCS fan (non-failed) to ON