Reviewer Flashcards

1
Q

(?) is mechanically similar to the brake-turbine arrangement. In this case however, the turbine drives a large centrifugal fan instead of a normal compressor.

A

TURBO-FAN TYPE

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2
Q

the difference between the air pressure inside the cabin and the air pressure outside the cabin.

A

CABIN DIFFERENTIAL PRESSURE

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3
Q

When ignited, it produces oxygen as it burns. This can be filtered and delivered through a hose to a mask that can be worn and breathed directly by the user.

A

SODIUM CHLORATE

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4
Q

is also known as barometric pressure and is measured with a barometer.

A

ATMOSPHERIC PRESSURE

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5
Q

is a colorless, odorless, and tasteless gas at normal atmospheric temperatures and pressures. It transforms into a liquid at -183 °C (its boiling point).

A

OXYGEN

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6
Q

is considered part of Earth’s atmosphere, but air density is so low that most of this layer is what is normally thought of as outer space.

A

THERMOSPHERE

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7
Q

can be used as an alternative to the air cycle cooling system. Although not commonly used these days for air conditioning systems, the system may be used as the means to remove heat from electrical and electronic equipment.

A

VAPOUR CYCLE COOLING SYSTEM

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8
Q

This system is used most frequently by the crew on high performance and air transport category aircraft.

A

DEMAND FLOW SYSTEM

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9
Q

is used to induce air across the condenser matrix when the aircraft is stationary on the ground and no ram air is available.

A

CONDENSER FAN

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10
Q

occurs when carbon monoxide builds up in your bloodstream.

A

CARBON MONOXIDE POISONING

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11
Q

are used to prevent the over pressurization of the aircraft cabin. They open at a preset differential pressure and allow air to flow out of the cabin.

A

PRESSURIZATION SAFETY VALVES

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12
Q

The valve for mixing is controlled in the cockpit or cabin by a

A

TEMPERATURE SELECTOR

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13
Q

This special container is used to store and transport liquid oxygen. It uses an evacuated, double-walled insulation design to keep the liquid oxygen under pressure at a very low temperature.

A

DEWAR BOTTLE

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14
Q

During ground operations and prior to takeoff, the (?) typically controls the position of the pressurization safety valve, which is held in the open position until the aircraft takes off.

A

WOW SWITCH

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15
Q

Liquids with a (?) have a stronger tendency to evaporate at normal temperatures than those with a high boiling point.

A

LOW BOILING POINT

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16
Q

These are components within the air conditioning system that transfer heat from one gas stream to another.

A

HEAT EXCHANGERS

17
Q

given the air pressure inside the cabin, the altitude on a standard day that has the same pressure as that in the cabin.

A

CABIN ALTITUDE

18
Q

the rate of change of air pressure inside the cabin, expressed in feet per minute (fpm) of cabin altitude change.

A

CABIN RATE OF CLIMB

19
Q

A (?) is used to prevent ground source air from flowing upstream into the air conditioning system.

A

CHECK VALVE

20
Q

acts as a reservoir and provides storage for the refrigerant, normally a highly volatile chemical such as Freon.

A

LIQUID RECEIVER

21
Q

This mode works to maintain cabin altitude at a single pressure despite the changing altitude of the aircraft.

A

ISOBARIC MODE

22
Q

Mixing (?) with bleed air in a duct or a mixing chamber allows the crew to select the exact temperature desired for the cabin.

A

AIR-CONDITIONED AIR

23
Q

A key factor in (?) is the ability of the fuselage to withstand the forces associated with the increase in pressure inside the structure versus the ambient pressure outside.

A

PRESSURIZATION

24
Q

The second most prevalent substance in the atmosphere

A

OXYGEN

25
Q

what does WOW stand for? *

A

WEIGHT ON WHEELS

26
Q

This also provides automatic control of pressurization, usually with different inputs, a standby controller, or standby outflow valve operation.

A

STANDBY MODE

27
Q

provides cooling when the pressure of the charge air is reduced by increasing its velocity and expanding it across the turbine of a so-called Air Cycle Machine.

A

EXPANSION

28
Q

composed principally of 78 percent nitrogen and 21 percent oxygen.

A

ATMOSPHERE/ AIR

29
Q

it can be used with the aircraft stationary on the ground with the aircraft engines running. It does not need to rely solely on ram air as the cooling medium for the pre-cooler.

A

TURBO-FAN

30
Q

This is achieved by using the charge air to drive a turbine, which is connected by a shaft to the compressor or fan within the cold air unit, thus converting heat energy into kinetic energy.

A

ENERGY CONVERSION

31
Q

the second layer. It starts above the troposphere and ends about 31 miles (50 km) above ground.

A

STRATOSPHERE

32
Q

is tested for the presence of water. This is done to avoid the possibility of it freezing in the small passage ways of valves and regulators.

A

AVIATOR’S BREATHING OXYGEN

33
Q

the highest layer, is extremely thin and is where the atmosphere merges into outer space.

A

EXOSPHERE

34
Q

Once in flight, the (?) automatically controls the sequence of operation of the pressurization components until the aircraft lands.

A

PRESSURIZATION CONTROLLER

35
Q

is used as the cooling medium to cool the very hot charge air ducted from the engine compressor or the gearbox mounted air compressor or blower.

A

RAM AIR