問題一覧
1
Engine compressor bleed air
2
heat exchanger
3
Provides cabin ventilation and increase or boosts pressure during high system demand or low pack flow
4
To recirculate the cabin air
5
To recirculate air supplied by the air conditioning packs
6
Improves air flow through the system without placing undue load on the air sources.
7
The aircraft exhaust pipe has a heater shroud around it. Outside air goes through the shroud and is heated up. It then goes to the cabin for heat. It is critical that the shroud is inspected for leaks So that no deadly carbon gets into cabin
8
the heater burns fuel from the aircraft fuel system to heat air coming from outside the plane. this now warmed air flows to the cabin where it provides heat.
9
aircraft fuel system
10
Ventilating fan – moves ambient air into outer cylinder when ram air is not available.
11
also known as “safety backup 2” shuts off fuel solenoid and ignition when it senses overheating
12
operates on transfer of heat, has both high and low side
13
•High side “ is where the refrigerant vapor is compressed to high pressure and gives up heat through the condenser” •low side “ accepts the heat because the refrigerant is at a low temperature and low pressure. low side begins at thermal expansion valve”
14
removes heat from the vapour and liquifies the gas into a high pressure liquid
15
pressure of both high and low sides, pressure indication on both high and low, depressurizing of both and high and low sides.
16
refrigerant turbine
17
used as cooling medium or coolant
18
the compressor drops the temperature and pressure of the air, that energy is used to drive the compressor
19
breathing comfort and ability to breath without supplemental oxygen.
20
the difference in pressure between pressure between the inside of the plane and outside of the plane
21
the outflow valve controls amount of “cabin pressure”. it is the major pressurization control
22
relieves cabin pressure to prevent max cabin differential pressure limits from being exceeded.
23
Plug type
24
cabin pressure and dynamic pressure test
25
14,000 ft and above
26
additionally processed to remove most of oxygens water content, this prevents freezing of the oxygen at cold temps and high altitudes
27
15 minutes
28
Green
29
oil and grease must not come into contact with nitrogen. keep containers clean
30
soapy solution used to find bubbles
31
life limit, manufacturing date/ expiry
32
at any temperature outside, summer or winter
33
formed by super cooled droplets rapidly freezing on impact
34
ice can form on engine air inlets, loss of lift and rotor vibration will occur
35
the aircraft will drastically lose lift due to poor airflow over the wing
36
looks like a small aircraft wing with a small probe sticking out the wing tip. when ice builds on that tip is slows the tips vibration in the wind. this indicates there is ice buildup. the system will melt that ice and re-run the test and keep checking.
37
flat black painted patch on leading edge of wing
38
allows ice to form, then expands and breaks the ice as it inflates
39
used for power plant anti icing
40
2 steps, type 1 applied hot, type 4 applied cold
41
wiper blades or use of water repellant spray that repels water droplets. spray called “rain-boe”
42
oxygen, heat, fuel
43
Class A; common materials “paper” Class B; flammable liquids “Avgas” Class C; electric fires Class D; combustible metals “wheels”
44
fire blocking materials used in seats and liners used around fueselage. track lighting in the ground and emergency exits clearly visible
45
the chance of a static shock is high, make sure refuelling unit is electrically bonded to plane before starting fueling.
46
class B
47
remove one of three elements that cause a flame to occur and be sustained. oxygen, heat, fuel
48
water is good for type A fires like wood, paper.
49
metal that is combustible, magnesium wheel hub
50
dry powder fire extinguishers are highly effective with class D fire
51
number of atoms for each element in the compound
52
CFC depletes ozone and is bad for the environment, new planes shifting to a more eco friendly method
53
class B and class C
54
the amount of airflow the moves through that zone, the more air flow = more oxygen which results in a larger fire
55
wheel wells where there is little to no air flow
56
consists of individually placed fire detectors or switches in high prone fire areas
57
2 independent loops that cover a large area, acts as a switch
58
locating overheating that could lead to a fire or fires started in areas beyond the line of sight. gives pilots good awareness of planes health
59
uses cartridges known as “squibs” that activate the slug through an explosion and activates the fire extinguisher
60
has its own air compressor when aircraft is NOT pressurized, can be filled and pressurized from water service panel outside fueselage
61
it is independent from planes systems
62
differential pressure creates a vacuum that sucks the shit outta the plane. a vacuum generator is also used
63
HALON 1301
64
it is a handheld fire extinguisher good for use inside the cabin, safe for humans in small amounts
65
class B and C fires
66
A- large amounts of airflow (piston engine) B-large amount of airflow (turbine engine cowling) C-relatively low airflow (APU) D-little to no air flow (wheel well bay) x- extremely high airflow, though to put out fires
67
warm fuel in the wings causes frost to form on top and underneath aircraft wings that freezes
68
PACK
69
a manifold set is required for servicing
70
RAM air, used to remove heat
71
the valve opens when cabin pressurization reaches an unsafe limit
72
cabin pressure dynamic test, aircraft is pressurized to 2 psi above atmospheric pressure.
73
ice to form, even on a warm day
74
deicing with heated fluid type1 type 4 anti icing applied after to prevent ice buildup
Composites test 2
Composites test 2
Zachary Halycz · 54問 · 2年前Composites test 2
Composites test 2
54問 • 2年前Systems test 2, 2023
Systems test 2, 2023
Zachary Halycz · 49問 · 2年前Systems test 2, 2023
Systems test 2, 2023
49問 • 2年前History test 1
History test 1
Zachary Halycz · 52問 · 2年前History test 1
History test 1
52問 • 2年前Composites and material test 1
Composites and material test 1
Zachary Halycz · 41問 · 2年前Composites and material test 1
Composites and material test 1
41問 • 2年前Systems test 2, 2023
Systems test 2, 2023
Zachary Halycz · 49問 · 2年前Systems test 2, 2023
Systems test 2, 2023
49問 • 2年前Electricity test 2
Electricity test 2
Zachary Halycz · 35問 · 2年前Electricity test 2
Electricity test 2
35問 • 2年前Engines test 1 good copy
Engines test 1 good copy
Zachary Halycz · 45問 · 2年前Engines test 1 good copy
Engines test 1 good copy
45問 • 2年前Composites test 2
Composites test 2
Zachary Halycz · 63問 · 2年前Composites test 2
Composites test 2
63問 • 2年前Engines test 2
Engines test 2
Zachary Halycz · 56問 · 2年前Engines test 2
Engines test 2
56問 • 2年前Basic systems, sem 2, test 1
Basic systems, sem 2, test 1
Zachary Halycz · 61問 · 2年前Basic systems, sem 2, test 1
Basic systems, sem 2, test 1
61問 • 2年前History test 1
History test 1
Zachary Halycz · 52問 · 2年前History test 1
History test 1
52問 • 2年前Electricity test 2
Electricity test 2
Zachary Halycz · 35問 · 2年前Electricity test 2
Electricity test 2
35問 • 2年前Composites test 2
Composites test 2
Zachary Halycz · 54問 · 2年前Composites test 2
Composites test 2
54問 • 2年前Engines test 2
Engines test 2
Zachary Halycz · 60問 · 2年前Engines test 2
Engines test 2
60問 • 2年前Engines test 1 good copy
Engines test 1 good copy
Zachary Halycz · 41問 · 2年前Engines test 1 good copy
Engines test 1 good copy
41問 • 2年前Structures sem 2, test 1
Structures sem 2, test 1
Zachary Halycz · 50問 · 2年前Structures sem 2, test 1
Structures sem 2, test 1
50問 • 2年前Basic systems test 4 final
Basic systems test 4 final
Zachary Halycz · 17問 · 3年前Basic systems test 4 final
Basic systems test 4 final
17問 • 3年前Basic systems, sem 2, test 1
Basic systems, sem 2, test 1
Zachary Halycz · 67問 · 2年前Basic systems, sem 2, test 1
Basic systems, sem 2, test 1
67問 • 2年前Electricity sem 2, test 1
Electricity sem 2, test 1
Zachary Halycz · 31問 · 2年前Electricity sem 2, test 1
Electricity sem 2, test 1
31問 • 2年前Structures test 2, memorization
Structures test 2, memorization
Zachary Halycz · 11問 · 2年前Structures test 2, memorization
Structures test 2, memorization
11問 • 2年前問題一覧
1
Engine compressor bleed air
2
heat exchanger
3
Provides cabin ventilation and increase or boosts pressure during high system demand or low pack flow
4
To recirculate the cabin air
5
To recirculate air supplied by the air conditioning packs
6
Improves air flow through the system without placing undue load on the air sources.
7
The aircraft exhaust pipe has a heater shroud around it. Outside air goes through the shroud and is heated up. It then goes to the cabin for heat. It is critical that the shroud is inspected for leaks So that no deadly carbon gets into cabin
8
the heater burns fuel from the aircraft fuel system to heat air coming from outside the plane. this now warmed air flows to the cabin where it provides heat.
9
aircraft fuel system
10
Ventilating fan – moves ambient air into outer cylinder when ram air is not available.
11
also known as “safety backup 2” shuts off fuel solenoid and ignition when it senses overheating
12
operates on transfer of heat, has both high and low side
13
•High side “ is where the refrigerant vapor is compressed to high pressure and gives up heat through the condenser” •low side “ accepts the heat because the refrigerant is at a low temperature and low pressure. low side begins at thermal expansion valve”
14
removes heat from the vapour and liquifies the gas into a high pressure liquid
15
pressure of both high and low sides, pressure indication on both high and low, depressurizing of both and high and low sides.
16
refrigerant turbine
17
used as cooling medium or coolant
18
the compressor drops the temperature and pressure of the air, that energy is used to drive the compressor
19
breathing comfort and ability to breath without supplemental oxygen.
20
the difference in pressure between pressure between the inside of the plane and outside of the plane
21
the outflow valve controls amount of “cabin pressure”. it is the major pressurization control
22
relieves cabin pressure to prevent max cabin differential pressure limits from being exceeded.
23
Plug type
24
cabin pressure and dynamic pressure test
25
14,000 ft and above
26
additionally processed to remove most of oxygens water content, this prevents freezing of the oxygen at cold temps and high altitudes
27
15 minutes
28
Green
29
oil and grease must not come into contact with nitrogen. keep containers clean
30
soapy solution used to find bubbles
31
life limit, manufacturing date/ expiry
32
at any temperature outside, summer or winter
33
formed by super cooled droplets rapidly freezing on impact
34
ice can form on engine air inlets, loss of lift and rotor vibration will occur
35
the aircraft will drastically lose lift due to poor airflow over the wing
36
looks like a small aircraft wing with a small probe sticking out the wing tip. when ice builds on that tip is slows the tips vibration in the wind. this indicates there is ice buildup. the system will melt that ice and re-run the test and keep checking.
37
flat black painted patch on leading edge of wing
38
allows ice to form, then expands and breaks the ice as it inflates
39
used for power plant anti icing
40
2 steps, type 1 applied hot, type 4 applied cold
41
wiper blades or use of water repellant spray that repels water droplets. spray called “rain-boe”
42
oxygen, heat, fuel
43
Class A; common materials “paper” Class B; flammable liquids “Avgas” Class C; electric fires Class D; combustible metals “wheels”
44
fire blocking materials used in seats and liners used around fueselage. track lighting in the ground and emergency exits clearly visible
45
the chance of a static shock is high, make sure refuelling unit is electrically bonded to plane before starting fueling.
46
class B
47
remove one of three elements that cause a flame to occur and be sustained. oxygen, heat, fuel
48
water is good for type A fires like wood, paper.
49
metal that is combustible, magnesium wheel hub
50
dry powder fire extinguishers are highly effective with class D fire
51
number of atoms for each element in the compound
52
CFC depletes ozone and is bad for the environment, new planes shifting to a more eco friendly method
53
class B and class C
54
the amount of airflow the moves through that zone, the more air flow = more oxygen which results in a larger fire
55
wheel wells where there is little to no air flow
56
consists of individually placed fire detectors or switches in high prone fire areas
57
2 independent loops that cover a large area, acts as a switch
58
locating overheating that could lead to a fire or fires started in areas beyond the line of sight. gives pilots good awareness of planes health
59
uses cartridges known as “squibs” that activate the slug through an explosion and activates the fire extinguisher
60
has its own air compressor when aircraft is NOT pressurized, can be filled and pressurized from water service panel outside fueselage
61
it is independent from planes systems
62
differential pressure creates a vacuum that sucks the shit outta the plane. a vacuum generator is also used
63
HALON 1301
64
it is a handheld fire extinguisher good for use inside the cabin, safe for humans in small amounts
65
class B and C fires
66
A- large amounts of airflow (piston engine) B-large amount of airflow (turbine engine cowling) C-relatively low airflow (APU) D-little to no air flow (wheel well bay) x- extremely high airflow, though to put out fires
67
warm fuel in the wings causes frost to form on top and underneath aircraft wings that freezes
68
PACK
69
a manifold set is required for servicing
70
RAM air, used to remove heat
71
the valve opens when cabin pressurization reaches an unsafe limit
72
cabin pressure dynamic test, aircraft is pressurized to 2 psi above atmospheric pressure.
73
ice to form, even on a warm day
74
deicing with heated fluid type1 type 4 anti icing applied after to prevent ice buildup