Prelim Flashcards

1
Q

Examples of artificial environment system

A
  • Air Conditioning System

- Pneumatic System

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2
Q

Purpose of the artificial environment system

A

For the comfort of the passengers or to sustain their lives

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3
Q

Purpose of Cabin Environment System (3)

A
  • Passenger Comfort
  • Maintenance Comfort
  • Prolong the Aircraft Service
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4
Q

The pressure inside and outside the aircraft must be ___

A

Equal

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5
Q

Each type of aircraft will have specific requirements according to the altitudes and speeds at which the aircraft is flown.

A

Flight Physiology

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6
Q

Study of how the body and mind work in a flying environment.

A

Flight Physiology

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7
Q

Study of how our organs function. And what keeps them from functioning in an abnormal environment.

A

Flight Physiology

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8
Q

An integral part of human factors and safe flight.

A

Flight Physiology

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9
Q

It has a direct effect on human performance.

A

Flight Physiology

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10
Q

Turbine Engine powered aircraft are efficient at high altitudes, but the human body is unable to exist in this cold and oxygen-deficient air.

A

Atmosphere

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11
Q

Physical mixture of gases

A

Atmosphere

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12
Q

Percentage of oxygen

A

21%

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13
Q

Percentage of nitrogen

A

78%

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14
Q

Percentage of all other gases

A

1%

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15
Q

5 Layers of the Atmosphere

A
  • Troposphere
  • Stratosphere
  • Mesosphere
  • Thermosphere
  • Exosphere
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16
Q

The Layer of Atmosphere:

Layer closest to Earth’s surface.

A

Troposphere

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17
Q

The Layer of Atmosphere:

Layer closest to Earth’s surface.

A

Troposphere

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18
Q

The Layer of Atmosphere:

Cessna or smaller aircraft can be seen

A

Troposphere

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19
Q

The Layer of Atmosphere:

This is where the jet aircraft and weather balloons fly.

A

Stratosphere

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20
Q

The Layer of Atmosphere:

Larger aircraft and commercial aircraft.

A

Stratosphere

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21
Q

The Layer of Atmosphere:

Hard to study layer.

A

Mesosphere

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22
Q

The Layer of Atmosphere:

Scientists do know that meteors burn up in this layer.

A

Mesosphere

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23
Q

The Layer of Atmosphere:

Considered part of the Earth’s atmosphere.

A

Thermosphere

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24
Q

The Layer of Atmosphere:

Air density is low that most of this layer is what is normally thought of as outer space.

A

Thermosphere

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25
Q

The Layer of Atmosphere:

Aurora, spacecraft

A

Thermosphere

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26
Q

The Layer of Atmosphere:

Highest layer and extremely thin

A

Exosphere

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27
Q

The Layer of Atmosphere:

Where the atmosphere merges into outer space.

A

Exosphere

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28
Q

The Layer of Atmosphere:

Satellites

A

Exosphere

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29
Q

Must be continually supplied with food and oxygen.

A

Human Respiration and Circulation

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30
Q

Must have their waste carried away and removed from the body.

A

Human Respiration and Circulation

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31
Q

Human Respiration and Circulation:

The lungs expand and the atmospheric pressure forces air into fill them.

A

Understand

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32
Q

Human Respiration and Circulation:
Two importance considerations in providing sufficient oxygen:
o Enough oxygen
o Sufficient pressure

A

Prioritize

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33
Q

Human Respiration and Circulation:

Abnormal breathing if oxygen is not properly supplied.

A

Hypoxia (Flight)

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34
Q

To provide pure oxygen to supplement the ever-decreasing amount of oxygen available in the atmosphere.

A

Oxygen System

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35
Q

To pressurize the aircraft to create an atmosphere that is like experienced naturally at lower altitudes.

A

Oxygen System

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36
Q

Designed to store or to generate a supply of pure oxygen and to regulate, dilute as required, and then distribute that oxygen to crew or passengers.

A

Oxygen System

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37
Q

Types of Oxygen System:

At normal room temperature and pressure.

A

Compressed Gas

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38
Q

Types of Oxygen System:

Contained under pressure, usually in the cylinder.

A

Compressed Gas

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39
Q

Types of Oxygen System:

A device used to provide oxygen therapy to people that require greater oxygen concentrations.

A

Portable Oxygen Concentrator

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40
Q

Types of Oxygen System:

Acts as a nebulizer

A

Portable Oxygen Concentrator

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41
Q

Types of Oxygen System:

Oxygen can be made liquid by lowering the temperature to below -183 Celsius or by placing gaseous oxygen under pressure.

A

Liquid Oxygen System

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42
Q

One of the artificial environments

A

Aircraft Pressurization System

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43
Q

Achieved by directing air into the cabin from either the compressor section of a jet engine, from a turbo-supercharger, or from an auxiliary compressor.

A

Aircraft Pressurization System

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44
Q

Air is ___, and the aerodynamic drag is ___ in high altitudes.

A
  • thin

- low

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45
Q

Deals with compressed air or pressurized gas as a source of power.

A

Pneumatic

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46
Q

The gas that is used in a pneumatic system.

A

Air

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47
Q

Sources of pneumatic power, pressurized air:

A
  • Engine
  • APU
  • GPU
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48
Q

Sources of pneumatic power, pressurized air:

Provides enough air for combustion purposes and for the pneumatic system.

A

Engine

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49
Q

Sources of pneumatic power, pressurized air:

Airflow is continuously entering (relative wind)

A

Engine

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50
Q

Sources of pneumatic power, pressurized air:

Used most of the time to pressurized

A

Engine

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51
Q

Sources of pneumatic power, pressurized air:

Used when the engine starts because the engine does not have a continuous airflow yet.

A

APU

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52
Q

Sources of pneumatic power, pressurized air:

For emergency situations with limited power.

A

APU

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53
Q

Sources of pneumatic power, pressurized air:

If ___ is not enough ram air turbine can be a back-up

A

APU

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54
Q

Sources of pneumatic power, pressurized air:

If APU is not enough ____ can be a back-up

A

Ram Air Turbine

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55
Q

Sources of pneumatic power, pressurized air:

Delivered via connectors, the High-Pressure Ground Connectors.

A

GPU

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56
Q

Sources of pneumatic power, pressurized air:

Ground power unit

A

GPU

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57
Q

Sources of pneumatic power, pressurized air:

External power

A

GPU

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58
Q

Sources of pneumatic power, pressurized air:

Used in ground only

A

GPU

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59
Q

Sources of pneumatic power, pressurized air:

Used for maintenance

A

GPU

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60
Q

On aircraft pneumatic energy is used for: (5)

A
  • Engine starting
  • Cabin pressurization and air conditions
  • Wing anti-icing
  • Water reservoir pressurization
  • Hydraulic reservoir pressurization
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61
Q

Reciprocating Engine Aircraft:

Pressurization air for smaller piston-engine aircraft is provided by ___ from the engine turbochargers.

A

Bleed air

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62
Q

Turbine Engine Aircraft:

A good source of air to pressurize the cabin.

A

Compressor

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63
Q

Turbine Engine Aircraft:

The air from the compressor in a turbine engine provides ___ aside from pressurization.

A

Heat

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64
Q

Turbine Engine Aircraft:

___ may be used directly, or it may be used to drive a turbo compressor.

A

Compressor bleed air

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65
Q

Electronic regulators and electrically actuated outflow valves perform the same function as pneumatic systems, only the ____ is different.

A

Power source

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66
Q

Electrical signals are sent to the cabin pressure controller from the cockpit control panel to set the:
o Mode of operation,
o Desired cabin altitude
o Either standard or local barometric pressure.

A

Electronic Regulators

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67
Q

Electronic Regulators:

Electrical signals are sent to the cabin pressure controller from the cockpit control panel to set the:

A

o Mode of operation,
o Desired cabin altitude
o Either standard or local barometric pressure.

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68
Q

To keep the aircraft cabin pressure at a safe level, any incoming air is held within the cabin.

A

Outflow Valve

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69
Q

The engines produce ___ to fly the aircraft.

A

Thrust

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70
Q

If ___ is increased pressure increases as well.

A

Thrust

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71
Q

If thrust is increased ___ increases as well.

A

Pressure

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72
Q

2 Valves of Pneumatic System Schematic

A
  • Pressure Regulator/Bleed Valve

* Built-In Pre-cooler (Fan-Air Valve)

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73
Q

Distribution Components

A
  • Wing duct (left and right)
  • Pylon duct (left and right)
  • APU duct
  • Crossover duct (cross bleed manifold)
  • Pneumatic ducts
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74
Q

Distribution Components:

Crossover duct is also known as

A

Cross bleed manifold

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75
Q

Distribution Components:

The pneumatic ducts are monitored by a?

A

Leak Detection System

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76
Q

Pressurization and Zones:

Areas that are pressurized:

A
  • Cockpit
  • Passenger compartment
  • Avionics computer and cargo
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77
Q

Pressurization and Zones:

Areas that are not pressurized

A
  • Radome
  • Landing gear bays
  • Tail cone
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78
Q

A flight hazard that destroys the smooth airflow across the aircraft’s lifting and control surfaces.

A

Ice

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79
Q

A flight hazard that decreases their ability to produce lift, increases the weight of the aircraft, and increases induced drag.

A

Ice

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80
Q

A hazard that affects the pilot’s ability to see clearly.

A

Rain

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81
Q

Deals with the operating and maintaining of aircraft ice prevention and removal system.

A

Ice and Rain Protection

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82
Q

Deals with procedures and equipment for ground ice and snow removal.

A

Ice and Rain Protection

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83
Q

Ice Formation and Classification:

This is reduced when the aircraft operates in the rain during take-off or approach.

A

Reduce Visibility

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84
Q

Ice Formation and Classification:

To solve reduced visibility, there are two systems in the aircraft.

A

o A windshield wiper for each pilot

o A rain repellant system

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85
Q

Ice Formation and Classification:

The aerodynamic quality of the aircraft is reduced.

A

Ice Buildup

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86
Q

Ice Formation and Classification:

The aircraft weight increases

A

Ice Buildup

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87
Q

Ice Formation and Classification:

Effects of Ice Buildup

A

o The aerodynamic quality of the aircraft is reduced

o Its weight increases

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88
Q

Ice Formation and Classification:

The engine can also get problems and the ice can block the ____ for the air data system.

A

Probes

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89
Q

Ice Formation and Classification:

___ on the windshields will decrease the visibility more than the rain.

A

Ice

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90
Q

Ice Formation and Classification:

Types of ice differ in their way of building up and structure.

A

Classification of Ice

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91
Q

Ice Formation and Classification:

Clouds have no ice but have ___ water droplets.

A

Supercooled

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92
Q

Ice Formation and Classification:

When clouds’ water droplets hit the aircraft, they change from ___ to ___.

A
  • Liquid water

- Solid ice

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93
Q
Ice Formation and Classification:
It affects the following aircraft parts:
o	Wings airplanes
o	Rotors of helicopters
o	Propellers
o	Stabilizer of airplanes
o	Stabilizers of helicopters
A

Clear Ice or Glaze

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94
Q

Ice Formation and Classification:

This is produced when temperature of the droplets is between 0 and -10 degrees Celsius.

A

Clear Ice or Glaze

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95
Q

Ice Formation and Classification:

Where does the ice buildup (clear ice) begins?

A

Leading edge of the surface.

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96
Q

Ice Formation and Classification:

This is produced when the temperature of the droplets is below -10 degrees Celsius.

A

Rime Ice

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97
Q

Ice Formation and Classification:

These are very cold droplets that freeze immediately and build up on the leading edge only.

A

Rime Ice

98
Q

Ice Formation and Classification:

When you fly at a higher speed in this condition, the rime ice layer forms a typical ____ shape.

A

Double horn

99
Q

Ice Formation and Classification:

Builds on the surface of aircraft that are packed outside in the cold nights.

A

Frost

100
Q

Ice Formation and Classification:

Frosts can have negative effects: (3)

A

o Decrease of lift
o Increase of weight
o Increase of drag

101
Q

These are pieces of dirt that may damage the fan blades or inlet blades.

A

Engine Ice Formation

102
Q

A disturbed airflow reduces the performance of the engine and can lead to a ___.

A

Compressor stall

103
Q

Ice Formation and Classification (6)

A
  • Reduce Visibility
  • Ice Buildup
  • Classification of Ice
  • Clear Ice or Glaze
  • Rime Ice
  • Frost
104
Q

Types of Oxygen (3)

A
  • Compressed Gas
  • Portable Oxygen Concentrator
  • Liquid Oxygen System
105
Q

Types of Ice Detection (3)

A
  • Thermal Anti-Ice System
  • Electronic Ice Detector
  • Optical Ice Detector
106
Q

Types of Ice Detection:

Can only do their task when they are switched on before any ice build-ups during flights.

A

Thermal Anti-Ice System

107
Q

Types of Ice Detection:
It is not permitted to keep this system on all the time. Because taking hot air from the engines reduces their performance and economy.

A

Thermal Anti-Ice System

108
Q

Types of Ice Detection:

It works by manually pressing the corresponding buttons on the control panel.

A

Thermal Anti-Ice System

109
Q

Types of Ice Detection:
Thermal Anti-Ice System -
Source of thermal air

A

Pneumatic and electrical air

110
Q

Types of Ice Detection:

Installed near the air data probes and therefore not visible to the pilot.

A

Electronic Ice Detector

111
Q

Types of Ice Detection:
When this component detects ice, it generates a message in the cockpit and can automatically activate the ice protection system.

A

Electronic Ice Detector

112
Q

Types of Ice Detection:

Visual indicator

A

Optical ice Detector

113
Q

Types of Ice Detection:
When the pilots see ice on this detector, then there is probably ice on the other parts of the aircraft. Therefore, pilots must switch on the thermal anti-ice system.

A

Optical ice Detector

114
Q

Types of Ice Detection:

Front windscreens where it is in sight of both pilots.

A

Optical ice Detector

115
Q

Removal of ice buildup.

A

De-Icing

116
Q

Prevention of ice buildup.

A

Anti-Icing

117
Q

Ice protection that is mainly performed on the ground when the aircraft is made ready for its journey.

A

De-Icing

118
Q

Types of De-Icing (4)

A
  • Pneumatic De-Icing
  • Electrical De-Icing
  • Chemical De-Icing
  • Hot Air De-Icing
119
Q

Types of De-Icing:

Used in propeller-driven airplanes and some helicopters in flight.

A

Pneumatic De-Icing

120
Q

Types of De-Icing:
Pneumatic de-icing system usually uses this at the leading edges of the wing and the stabilizers, which normally have the shape of the leading-edge structure.

A

Rubber boots

121
Q

Types of De-Icing:

Used in some airplanes and some large helicopters in flight.

A

Electrical De-Icing

122
Q

Types of De-Icing:

Each heated stall has its own temperature control circuit.

A

Electrical De-Icing

123
Q
Types of De-Icing:
Its components are:
o	Heating mats in the slats
o	Control unit
o	Temperature sensors
A

Electrical De-Icing

124
Q

Types of De-Icing:

Components of Electrical De-Icing (3)

A

o Heating mats in the slats
o Control unit
o Temperature sensors

125
Q

Types of De-Icing:

Applied on airplanes to remove frost from the airfoil and the fuselage on the ground.

A

Chemical De-Icing

126
Q

Types of De-Icing:

Commonly performed in both commercial and general aviation.

A

Chemical De-Icing

127
Q

Types of De-Icing:

Chemical De-Icing fluids (2)

A

De-icing or anti-icing fluids

128
Q

Types of De-Icing:

Mixture of glycol and water

A

Chemical De-Icing

129
Q

Types of De-Icing:
Chemical De-Icing -
Prevents a new ice build-up for a limited time, depending on the weather conditions.

A

Anti-icing fluids

130
Q

Types of De-Icing:

Applied on airplanes to remove frost from specific devices on the ground.

A

Hot Air De-Icing

131
Q

Types of De-Icing:

Chemical de-icing can damage some engine types. For this reason, this system is used instead.

A

Hot Air De-Icing

132
Q

Types of De-Icing:
(Hot Air De-Icing)
Releases hot air

A

Hot air blower

133
Q

Types of De-Icing:

Other critical devices that may be damaged in de -icing process (3)

A

o APU inlet and exhaust
o Carbon Brakes
o Radome

134
Q

Ice protection that is mainly performed during flight.

A

Anti-Icing

135
Q

Types of Anti-Icing (5)

A
  • Pneumatic/Hot Air Anti-Icing
  • Hot Oil Anti-Icing
  • Chemical Anti-Icing
  • Electrical Anti-Icing
  • Telescoping Duct
136
Q

Types of Anti-Icing:

Applied in flight

A

Pneumatic/Hot Air Anti-Icing

137
Q

Types of Anti-Icing:
(Pneumatic/Hot Air Anti-Icing)
Uses hot air which is already regulated by the bleed valve of the pneumatic system.

A

Wing Anti-Ice

138
Q

Types of Anti-Icing:
(Pneumatic/Hot Air Anti-Icing)
Uses bleed air from the corresponding engine.

A

Engine Anti-Ice

139
Q

Types of Anti-Icing:
(Pneumatic/Hot Air Anti-Icing)
Must make sure that ice pieces from the fuselage do not hit the engine.

A

Centre Engines

140
Q

Types of Anti-Icing:

Used in some small airplanes after and in helicopters

A

Hot Oil Anti-Icing

141
Q

Types of Anti-Icing:

Used for engine anti-icing

A

Hot Oil Anti-Icing

142
Q

Types of Anti-Icing:

This system leads the hot oil from the engine through hollow struts in the engine air intake.

A

Hot Oil Anti-Icing

143
Q

Types of Anti-Icing:

The struts heat up to prevent icing of the air intake area.

A

Hot Oil Anti-Icing

144
Q

Types of Anti-Icing:

Applied on airplanes after de-icing on ground and on some propeller driven airplanes in flight.

A

Chemical Anti-Icing

145
Q

Types of Anti-Icing:

Used in some propeller-driven aircraft

A

Chemical Anti-Icing

146
Q

Types of Anti-Icing:

Used in all aircraft in flight

A

Electrical Anti-Icing

147
Q

Types of Anti-Icing:

A probe heat system prevents blocking of data probes.

A

Electrical Anti-Icing

148
Q

Types of Anti-Icing:
(Electrical Anti-Icing)
It prevents blocking of data probes.

A

Probe heat system

149
Q

Types of Anti-Icing:

A window heat system prevents ice on the windshield that would reduce visibility.

A

Electrical Anti-Icing

150
Q

Types of Anti-Icing:

A line and drain mast heat system prevents frozen water lines.

A

Electrical Anti-Icing

151
Q

Types of Anti-Icing:
(Electrical Anti-Icing)
It prevents ice on the windshield that would reduce visibility.

A

Window heat system

152
Q

Types of Anti-Icing:
(Electrical Anti-Icing)
It prevents frozen water lines.

A

Line and drain mast heat system

153
Q

Types of Anti-Icing:

Necessary to supply the wing anti-ice duct.

A

Telescoping Duct

154
Q

Types of Anti-Icing:

Is short when the slats are retracted

A

Telescoping Duct

155
Q

Types of Anti-Icing:

Is long when slats are extended.

A

Telescoping Duct

156
Q

Types of Anti-Icing:

Used for jet aircraft/engines

A

Telescoping Duct

157
Q

Types of Anti-Icing:

Telescoping Duct is ___ when the slats are retracted.

A

short

158
Q

Types of Anti-Icing:

Telescoping Duct is ___ when slats are extended.

A

long

159
Q

Types of Anti-Icing:

Telescoping Duct is short when the slats are ___.

A

retracted

160
Q

Types of Anti-Icing:

Telescoping Duct is long when slats are ___.

A

extended

161
Q

Results of Ice Buildup (6)

A
  • Poor aerodynamic
  • More aircraft weight
  • Engine problems
  • Blocked air data probes
  • Reduced visibility
  • Frozen water lines
162
Q

Rain Removal Systems (2)

A
  • Windshield wiper

- Rain Repellant

163
Q

Rain Removal Systems:

Removes water mechanically.

A

Windshield Wiper

164
Q

Rain Removal Systems:

Rain repellant fluid or special windshield coating.

A

Rain Repellant

165
Q

Rain Removal Systems:

Mixture of glycol and water

A

Rain Repellant

166
Q

Rain Removal Systems:

Rain Repellant is a mixture of

A

Glycol and water

167
Q

Aircraft Oxygen Systems (3)

A
  • Crew oxygen system
  • Passenger oxygen system
  • Portable oxygen system
168
Q

A system that is used when there is depressurization or accidents.

A

Aircraft Oxygen System

169
Q

As the altitude increases the air pressure and density of air ____.

A

Decreases

170
Q

The volume you breathe stays the same but at about ___ ft. the amount of usable oxygen has halved.

A

18,000

171
Q

At this altitude, you would have trouble staying alive.

A

18,000 ft.

172
Q

At ___ ft. the amount of usable oxygen you inhale is about a quarter of that at sea level.

A

33,000

173
Q

Loss of cabin pressure.

A

Rapid decompression

174
Q

When the AC is cruising, the cabin pressure is maintained at about ____ ft.

A

8,000

175
Q

At what feet humans compensate for the lack of oxygen by breathing faster.

A

10,000 ft.

176
Q

At what feet the first effects of altitude will show, such as exhaustion and sleepiness.

A

14,000 ft.

177
Q

At what feet is the zone of incomplete compensation.

A

15,000-20,000 ft.

178
Q

At 15,000-20,000 ft. what are the zone of incomplete compensation

A
o	Loss of concentration
o	Partial memory loss
o	Feel a sense of well being
o	Muscle would ache 
o	Loss of judgment
179
Q

Types of Oxygen (3)

A
  • Aviators Breathing Oxygen
  • Medical Oxygen
  • Technical Oxygen
180
Q

At low temperatures, any moisture in our oxygen would ___.

A

freeze

181
Q

Characteristics of Oxygen:

Used on aircraft because it is very dry

A

Aviators Breathing Oxygen

182
Q

Characteristics of Oxygen:

Never used on aircraft as it contains water droplets and would therefore freeze.

A

Medical Oxygen

183
Q

Characteristics of Oxygen:

Used in the medical field.

A

Medical Oxygen

184
Q

Characteristics of Oxygen:

Should never be used for breathing as it is contaminated.

A

Technical Oxygen

185
Q

Characteristics of Oxygen:

Used in welding.

A

Technical Oxygen

186
Q

Characteristics of Oxygen:

For industrial work.

A

Technical Oxygen

187
Q

Characteristics of Oxygen (3)

A
  • Invisible/dry
  • Odorless
  • Non-flammable
188
Q

It supplies the cockpit crew with oxygen it is always available.

A

Crew Oxygen System

189
Q

Types of Aircraft Oxygen System:
It consists of 1 or more high-pressure oxygen bottles (4 maximum). These are stored in the lower deck, either in the avionics compartment or in the cargo compartment.

A

Crew Oxygen System

190
Q

Where does the crew oxygen system locate?

A

Avionics compartment or cargo compartment (typically on the left hand).

191
Q

Types of Aircraft Oxygen System:

Attached to each bottle is a pressure regulator.

A

Crew Oxygen System

192
Q

Oxygen is stored in cylinders known as ___.

A

Oxygen bottles

193
Q

Oxygen bottles are made up of? (2)

A
  • Steel alloy

- Composite material: Kevlar

194
Q

What color are oxygen bottles?

A

Dark Green

195
Q

Oxygen bottles store ___ psi.

A

1850-1900

196
Q

Each oxygen bottle has a slow-opening shut-off valve that opens and closes the bottle. The valve should either be ___.

A

fully opened or fully closed

197
Q

Oxygen Bottles:

A disk which is a safety device is also known as

A

Frangible Disk

198
Q

Oxygen Bottles:

If the frangible disk is damaged, what color will be shown in the discharge indicator?

A

Yellow

199
Q

Oxygen Bottles:

If the frangible disk is normal, what color will be shown in the discharge indicator?

A

Green

200
Q

Oxygen Bottles:

What does the direct reading pressure gauge indicate?

A

The bottle pressure

201
Q

Oxygen Bottles:

What indicates the bottle pressure?

A

The direct reading pressure gauge

202
Q

Oxygen Bottles:

What controls the psi that will flow to the oxygen mask of the pilots.

A

Pressure regulator transmitter assembly

203
Q

Oxygen Bottles:

What is the pressure range of the oxygen received by pilots?

A

65-94 psi.

204
Q

Oxygen Bottles:

What shows the psi of the oxygen bottle?

A

Door/Oxy ECAM page

205
Q

Oxygen Bottles:

What is the use of the door/oxy ECAM page?

A

It shows the psi of the oxygen bottle.

206
Q
  • The oxygen is transported to the cockpit via lines and manifold.
  • A pressure regulator is located near the oxygen bottles to reduce the length of high-pressure lines.
A

Distribution

207
Q

Distribution:

The oxygen is transported to the cockpit via ____.

A

lines and manifold

208
Q

Distribution:

A pressure regulator is located near the oxygen bottles to reduce the ____.

A

length of high-pressure lines

209
Q

Distribution:

Where is the pressure regulator located?

A

Near the oxygen bottles

210
Q

Distribution:

Green indication

A

Normal

211
Q

Distribution:

Amber indication

A

Low pressure

212
Q

Distribution:

Yellow indication

A

Overpressure

213
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
Has a microphone connector.

A

Crew Oxygen Mask

214
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
How many seconds can a flight crew put their mask on?

A

5 seconds

215
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
• The mask itself consists of a quick donning mask:

A

o Harness (inflatable)
o Facepiece
o Microphone

216
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
Diluter demand regulator (3 selection)

A
  • Normal
  • 100% oxygen
  • Emergency
217
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
Crew Oxygen Mask parts (5)

A
  • Smoke goggles
  • Integrated microphone
  • Harness inflation control valve
  • Press to test/emergency knob
  • N-100% lever
218
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
Pull the grip of the mask to inflate the harness

A

Access

219
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
Where is the crew oxygen mask located?

A

Stowage box, side console (near the armrest of the pilot)

220
Q

Types of Aircraft Oxygen System:
Pilot of Crew Oxygen System:
Where is the location of the crew oxygen bottle?

A

Lower deck or avionics compartment

221
Q

Types of Aircraft Oxygen System:

It is only used if the cabin depressurized.

A

Passenger Oxygen System

222
Q

Types of Aircraft Oxygen System:
Passenger Oxygen System:
Where are oxygen masks located?

A
  • Every seat (passenger service unit)
  • All lavatories
  • Every attendant station
223
Q

Types of Aircraft Oxygen System:
Passenger Oxygen System:
PSU means

A

Passenger service unit

224
Q

Types of Aircraft Oxygen System:
Passenger Oxygen System:
It is ____ supplied if cabin depressurization occurs.

A

automatically

225
Q

Types of Aircraft Oxygen System:
Passenger Oxygen System:
How long is the oxygen supply available?

A

15 minutes

226
Q

Types of Aircraft Oxygen System:
Passenger Oxygen System:
System activation

A
  • The system is normally activated automatically by a pressure switch in the pressurized area.
  • Manually switch the “masked man on”.
  • The flight crew can use the manual release tool to activate the oxygen supply
  • Must be pulled by the passengers
227
Q

Types of Aircraft Oxygen System:
Passenger Oxygen System:
2 ways that oxygen is supplied to the system

A
  • Chemical System

- Gaseous System

228
Q

Types of Aircraft Oxygen System:

Normally stored in the cockpit and near the exits in the passenger compartment.

A

Portable Oxygen System

229
Q

Types of Aircraft Oxygen System:

It provides a portable supply of breathing oxygen that is independent of the fixed systems.

A

Portable Oxygen System

230
Q

Types of Aircraft Oxygen System:

It is intended for emergency and first-aid use.

A

Portable Oxygen System

231
Q

Types of Aircraft Oxygen System:

2 types of Portable Oxygen Systems

A
  • Portable breathing equipment (PBE)

- Portable oxygen bottle

232
Q

Turbine Engine Aircraft:

A good source of air to pressurize the cabin.

A

Compressor in a turbine engine

233
Q

Turbine Engine Aircraft:

What does hot air provides? (2)

A

Pressurization and heat

234
Q

Turbine Engine Aircraft:

Compressor bleed air may be used (2)

A
  • Directly

- Drive a turbo compressor

235
Q

Turbine Engine Aircraft:

Used directly or may be used to drive a turbo compressor.

A

Compressor bleed air

236
Q

Turbine Engine Aircraft:

It flows through the nozzle of a jet pump at a high velocity.

A

Compressor bleed air

237
Q

Turbine Engine Aircraft:

It draws air in from the outside of the aircraft

A

Compressor bleed air

238
Q

Turbine Engine Aircraft:

Taken in and compressed

A

Outside air

239
Q

Turbine Engine Aircraft:

It is mixed with the engine compressor bleed air that has been used to drive the turbo compressor.

A

Outside air

240
Q

Turbine Engine Aircraft:

It enters the cabin after being mixed with engine compressor bleed air.

A

Outside air

241
Q

Turbine Engine Aircraft:

Process of the outside air before it enters the cabin (3)

A
  • Taken in
  • Compressed
  • Mixed with the engine compressor bleed air