Air Conditioning And Pressurization Flashcards

(30 cards)

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

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
How many recirculating fans are there, what do they do and how are they controlled
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
How and when would you introduce Ram air into the aircraft
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
What happens to the air conditioning system if an engine failure occurs above 13500ft? And below 13500ft
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
Is there anytime the automatic switch to economy flow will not work
Economy​ flow​ is inhibited when both temper-​ature control​ p/b’s are in manual​ mode and 1 pack is off
29
If an external air conditioning unit is supplying ventilated air, what precautions must you take and why
Open avionics hatch or cockpit windows before connecting the unit
30
What would you do to reduce cabin air temperature during ground ops and initial flight
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.