Air Conditioning And Pressurization Flashcards

1
Q

What is normally operating max differential pressure as applied by the controller

A

7.46 psi

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2
Q

At that differential pressure what is the cabin altitude at 35000 ft

A

8000ft

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3
Q

What is the diff pressure limited by the outflow valves

A

7.65

Cabin Alt limiting at 12500ft +/- 1500ft

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4
Q

What is the altitude limiter set to

A

12000ft +/- 1500ft

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5
Q

What warning is there of excessive cabin altitude

A

An excessive cabin Altitude warning is presented when the cabin Altitude reaches 10000ft

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6
Q

How is the fuselage protected against negative pressure

A

The cabin is automatically depressurised upon landing, two inward pressure relief valves prevent negative cabin pressure

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7
Q

How do you set the panel for automatic operation

A

Set the landing elevation and rate control knob in the datum.

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8
Q

What happens if the active Channel fails

A

The standby channel takes over, level 1 alert

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9
Q

How do you manually change channels on the controller

A

Pressing the PRESS CONTROL p/b twice in succession

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10
Q

What happens if both channels fail? What do you do

A

Manual mode is automatically activated and an alert is generated level 2 alert CAB PRESSURE CONTROL

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11
Q

How do you control pressurisation in manual

A

Bu selecting PRESS CONTROL p/b and the up and down toggle and decrease or increase the rate with the rate knob

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12
Q

What pressurisation alerts are there and at what level

A

CABIN PRESSURISATION CONTROLLER CHANEL FAULT- level 1
CABIN PRESSURISATION CONTROLLER FAULT—level 2
EXCESSIVE CABIN ALTITUDE— level 3

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13
Q

how many air conditioning packs are installed

A

Two, Pack 1 and Pack 2

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14
Q

Is a single pack enough to satisfy the requirements

A

Yes single pack can meet all requirements

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15
Q

Which pack supplies what area

A

Pack 1 serves Flightdeck

Pack 2 serves cabin

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16
Q

What conditions must be met for a pack valve to open

A

when pressure is >10 psi and system is on

17
Q

When will auto shutoff of both packs occur

A

Auto Shut-off​ of​ both packs occurs:​ ​- ​On the ground​ during engine starting or​ ​when both thrust​ reversers are unlocked.​ ​- ​If​ an engine failure is detected during​ ​take-​off​ or​ in flight​ at​ altitudes below​ ​ ​13 500 ft​ and a thrust​ lever​ setting above​ ​MIN​ TO is​ selected.​

18
Q

How is pack operation restored after an auto shutoff due to engine failure

A

In case of an auto shut-off​ due to engine fail-​ure,​ pack operation is restored by​ operating​ ​the​ AIRCOND AUTO SH​UT​ p/b located​ at​ ​ ​the ram​ air​ panel​ or by​ selecting a lower​ ​thrust​ lever​ setting. Pack​ operation​ will​ be​ ​automatically​ restored when climbing above​ ​13 500 ft

19
Q

How are normal and economy flows selected

A

There are three modes​ of​ flow​ control:​ nor-​ ​mal,​ economy and​ augmented.​ ​Normal​ and​ ​economy flows​ can​ be selected​ manually.​ ​Economy​ flow is​ obtained when both pack ​valves are open and the automatically​ con-​trolled cabin temperature is​ ​within a preset​ ​range​ from​ the​ selected​ temperature.​ Econ-​ ​omy​ flow​ is automatically​ selected:

20
Q

What is augmented flow

A

High output flow of 140%

21
Q

If you are in economy mode and a pack fails, what happens

A
22
Q

How do you select a cabin or Flightdeck temperature

A

The temperature may​ be controlled automat-​ically​ or manually​ via the temperature selec-​tors.​ The air​ temperature​ of​ cabin,​ cabin ​ ​supply, and flight​ deck supply​ can be dis-​played

23
Q

Where is air temperature displayed

A

The air​ temperature​ of​ cabin,​ cabin ​ ​supply, and flight​ deck supply​ can be dis-​played on the overhead panel

24
Q

How is the flight deck and cabin air distributed

A

Conditioned air from​ the manifold is distrib-​ ​uted to the flight deck​ and cabin via​ indepen-​dent​ ducts

25
Q

How many recirculating fans are there, what do they do and how are they controlled

A

4 fansCabin​ air​ is distributed​ overhead along​ each​ ​cabin wall.​ The cabin air​ can be recirculated​ ​ ​by​ four​ recirculation fans which are mounted​ ​ ​in the cabin ceiling. The fans are controlled​ ​ ​by​ the RECIRC​ FANS p/b’s

26
Q

How and when would you introduce Ram air into the aircraft

A

During unpressurized flight ram air may be introduced to the​ manifold via a valve. Control is by ​the RAM AIR p/b located at the ram air panel

27
Q

What happens to the air conditioning system if an engine failure occurs above 13500ft? And below 13500ft

A

On the ground​ during engine starting or​ ​when both thrust​ reversers are unlocked.​ ​- ​If​ an engine failure is detected during​ ​take-​off​ or​ in flight​ at​ altitudes below​ ​ ​13 500 ft​ and a thrust​ lever​ setting above​ ​MIN​ TO is​ selected.​ ​In case of an auto shut-off​ due to engine fail-​ure,​ pack operation is restored by​ operating​ ​the​ AIRCOND AUTO SH​UT​ p/b located​ at​ ​ ​the ram​ air​ panel​ or by​ selecting a lower​ ​thrust​ lever​ setting. Pack​ operation​ will​ be​ ​automatically​ restored when climbing above​ ​13 500 ft.

28
Q

Is there anytime the automatic switch to economy flow will not work

A

Economy​ flow​ is inhibited when both temper-​ature control​ p/b’s are in manual​ mode and 1 pack is off

29
Q

If an external air conditioning unit is supplying ventilated air, what precautions must you take and why

A

Open avionics hatch or cockpit windows before connecting the unit

30
Q

What would you do to reduce cabin air temperature during ground ops and initial flight

A

Low pressure conditioned air can be supplied to the manifold for distribution throughout the ​aircraft via​ a​ ground connection provided at the forward right section of the aircraft.