ATA 21 Environmental Control Systems Flashcards

1
Q

How many condition packs are there?

A

2 - each one with a three-wheel ACM

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2
Q

What will happen if a double pack failure occurs?

A

Ambient air from the ram scoop will be ducted into the air distribution system

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3
Q

Where is the air conditioning panel located?

A

On the overhead panel in the cockpit

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4
Q

Where do the RH conditioning pack mainly provide its air?

A

To the cockpit

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5
Q

Where do the LH conditioning pack mainly provide its air?

A

To the cabin

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6
Q

How is the air to the cockpit supplied?

A

Through two overhead inlet air boxes attached to the left and right side of the forward face of the passenger and cockpit bulkhead

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7
Q

How is the air to the cabin supplied?

A

Through the left and right overhead ducts

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8
Q

How is the lavatory supplied with air?

A

Through a tapping of the right overhead duct

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9
Q

To which altitude can the pressurisation system keep take-off level?

A

12000 ft

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10
Q

What is the normal operating differential pressure?

A

7,0 psid

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11
Q

In which range can the temperature be selected in automatic operation?

A

18 to 29°C

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12
Q

What is used to prevent an imbalance of air flow temperature between LH and RH cooling packs outlets?

A

A turbulence generator

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13
Q

From where is the avionics rack ventilated?

A

A fan draws air from the cabin through a filter

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14
Q

When is main batteries ventilated?

A

On ground (when NLG down lock switch is activated)

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15
Q

Where is the recirculation filter installed?

A

Under the cabin floor

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16
Q

What happens if the avionic ventilating fan stops?

A

AVIONICS VENT will light up on the CWP

17
Q

When will the avionic ventilation fan operate at full speed?

A

If the temperature in the avionics rack rises above 36°C

18
Q

Where is cabin pressure control unit located?

A

Upper shelf of avionic rack

19
Q

When will warning CABIN PRESS indicate?

A

When the cabin altitude exceeds 10000 ft of the diff press exceeds 7,5 psi