AC ENVIRONMENT AND AUXILIARY SYSTEM Flashcards

1
Q

Aircraft are flown at high altitudes for TWO REASONS:

A

Consumes less fuel

Bad weather and turbulence

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2
Q

It is a process in which conditioned air is pumped into the cabin of an aircraft or spacecraft, in order to create a safe and comfortable environment for passengers and crew flying at high altitudes.

A

CABIN PRESSURIZATION

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3
Q

This prevents rapid changes of cabin altitude that may be uncomfortable or cause injury to passengers and crew.

A

CABIN PRESSURIZATION SYSTEM

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4
Q

A cabin pressurization system typically maintains a cabin pressure altitude of approximately __________ at the maximum designed cruising altitude of an aircraft.

A

8,000 FT.

(2,400 METER)

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5
Q

It is proportional to the pressure outside the aircraft, in order to reduce the stress in the aircraft fuselage.

A

CABIN PRESSURE

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6
Q

It is maintained while the aircraft is cruising at its max altitude then gradually reduces during the decent of the aircraft, until it matches
the ambient air pressure at the destination.

A

CABIN PRESSURE

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7
Q

the actual height above sea level at which the aircraft is flying

A

AIRCRAFT ALTITUDE

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8
Q

the temperature in the area immediately surrounding the aircraft.

A

AMBIENT TEMPERATURE

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9
Q

the pressure in the area immediately surrounding the aircraft .

A

AMBIENT PRESSURE

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10
Q

cabin pressure in terms of equivalent altitude above sea level.

A

CABIN ALTITUDE

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11
Q

the difference in pressure between the pressure acting on one side of a wall and the pressure acting on the other side of the wall

A

DIFFERENTIAL PRESSURE

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12
Q

PHYSIOLOGICAL PROBLEMS ARISING DUE TO FAILURE OF CABIN PRESSURIZATION

A

Hypoxia

Altitude sickness

Decompression sickness

Barotrauma

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13
Q

The lower partial pressure of oxygen at altitude reduces the alveolar oxygen tension in the lungs and subsequently in the brain, leading to sluggish thinking, dimmed vision, loss of consciousness, and ultimately death.

A

HYPOXIA

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14
Q

Hyperventilation, the body’s most common response to hypoxia, does help to partially restore the partial pressure of oxygen in the blood, but it also causes carbon dioxide (CO2) to out-gas, raising the blood pH and inducing alkalosis.

A

ALTITUDE SICKNESS

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15
Q

The low partial pressure of gases, principally nitrogen (N2) but including all other gases, may cause dissolved gases in the bloodstream to precipitate out, resulting in gas embolism, or bubbles in the bloodstream.

A

DECOMPRESSION SICKNESS

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16
Q

As the aircraft climbs or descends, passengers may experience discomfort or acute pain as gases trapped within their bodies expand or contract.

A

BAROTRAUMA

17
Q

It provides cabin pressure regulation, pressure relief, vacuum relief, and the means for selecting the desired cabin altitude in the isobaric and differential range.

A

CABIN PRESSURE CONTROL SYSTEM

18
Q

an outflow valve, and a safety valve are used to accomplish these functions.

A

CABIN PRESSURE REGULATOR

19
Q

It controls cabin pressure to a selected
value in the isobaric range and limits cabin pressure to a preset differential value in the differential range.

A

CABIN PRESSURE REGULATOR

20
Q

It is used to prevent the maximum differential
pressure, for which the fuselage was designed, from being exceeded.

A

DIFFERENTIAL CONTROL

21
Q

It is determined by the structural strength of the cabin and often by the relationship of the cabin size to the probable areas of rupture, such as window areas and doors.

A

DIFFERENTIAL PRESSURE

22
Q

It is a combination pressure relief vacuum relief, and dump valve.

A

CABIN AIR PRESSURE SAFETY VALVE

23
Q

It prevents cabin pressure from exceeding a pre determined differential pressure above ambient pressure.

A

PRESSURE RELIEF VALVE

24
Q

It prevents ambient pressure from exceeding cabin pressure by allowing external air to enter the cabin when ambient pressure exceeds cabin pressure.

A

VACUUM RELIEF

25
Q

It actuates the dump valve. When this switch is positioned to ram, a solenoid valve opens, causing the valve to dump cabin air into the atmosphere.

A

FLIGHT DECK CONTROL SWITCH

26
Q

It is designed to withstand a particular maximum cabin differential pressure.

A

FUSELAGE

27
Q

It indicates the difference between inside and outside pressure.

A

CABIN DIFFERENTIAL PRESSURE GAUGE

28
Q

This gauge should be
monitored to assure that the cabin does not exceed the maximum allowable differential pressure.

A

CABIN DIFFERENTIAL PRESSURE GAUGE

29
Q

It is also provided as a check on the performance of the system.

A

CABIN ALTIMETER

30
Q

Advantages of Cabin Pressurization System

A

Helps to maintain aircraft cabin pressure at high
altitudes.

It responds to minor changes in cabin pressure with respect to aircraft altitude.

It generates ambient atmosphere for passengers and prevents passengers from physiological problems.

It also maintains and monitor cabin air quality as per directed by World Health Organization (WHO).

31
Q

Disadvantages of Cabin Pressurization System

A

DECOMPRESSION

32
Q

It is defined as the inability of the aircraft’s
pressurization system to maintain its designed pressure differential.

A

DECOMPRESSION

33
Q

This can be caused by a malfunction in the
pressurization system or structural damage to the aircraft.

A

DECOMPRESSION

34
Q

two categories of decompression

A

Explosive decompression

Rapid decompression

35
Q

a change in cabin pressure in which the lungs decompress faster than the cabin.

A

RAPID DECOMPRESSION

36
Q

a change in cabin pressure faster
than the lungs can decompress, possibly resulting in lung damage.

A

EXPLOSIVE DECOMPRESSION