Aircraft Systems Flashcards

1
Q

Avgas used for?

A

Piston engines a/c or internal combustion engines a/c

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2
Q

Avtur and avgas equals

A

Avtag

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3
Q

Avtag is known as what’s? Avtur and gasoline

A

Wide cut fuel

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4
Q

Avcat is avtur and diesel used together and is used on?

A

Carriers

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5
Q

Avtur FSII stands for?

A

Fuel system icing inhibitor

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6
Q

Avcat with fsii is used on?

A

Carriers

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7
Q

Name the fuel system,

A

Fuel from main tank to collector tank by jet pump.

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8
Q

What is cross feeding?

A

Cross feed is when one tank feeds more than one engine

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9
Q

How do we move fuel from one tank to another?

A

Fuel transfer.

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10
Q

What colour are fuel warnings and cautions?

A

Red and amber

Warnings and cautions

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11
Q

What side is in the low pressure side of the airframe?

A

LP pump, LP fuel cock

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12
Q

Most commonly used fuel in gas turbine engines

A

Aftur or avtur fsii

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13
Q

Flash point of fuel is?

A

Lowest temp at which fuel can combust

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14
Q

What happens if you close the LP fuel cock?

A

Prevent fuel reaching the engine.

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15
Q

Parts of an engine?

A

Intake, compressor, combustion chamber, turbine, exhaust

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16
Q

Brayton cycle?

A

Induction, compression, combustion, exhaust. Compression goes up with pressure axis

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17
Q

Turbo fan engine is driven by what?

A

Low pressure turbine at the rear. It’s the last turbine and it drives the fan. It extracts sufficient energy from the gas to drive the fan

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18
Q

2 types of compressor

A

Centrifugal and axial

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19
Q

Centrifugal

A
Cheap
Easy to make
Low maintenance 
Small mass flow rates
Large frontal area
Air flows radially in the compressor 
Usually single stage 
86% efficient
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20
Q

Turbo prop

A

Gas turbine driving a propellor. Uses max energy from gas to drive propellor.

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21
Q

Propellor propulsive efficiency

Blue line is turbo prop

A

Blue line is turbo prop

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22
Q

Turbo prop drops off at 350 kts why?

A

Shockwaves at the tips.

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23
Q

Stall is what?

A

A partial breakdown of airflow through the compressor

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24
Q

Surge?

A

A total breakdown of airflow through the compressor

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25
Purpose of oil filter?
To remove debris from system
26
Boundary lubrication?
Surfaces are kept in contact
27
Hydrodynamic lubrication?
Layers are apart
28
Oil tank is what
Main storage for oil
29
Boundary layer lubrication appears where?
Start up
30
Left of fuel pump is low px right is high px
.
31
High pressure system components include?
Throttle valve FCU, HP shut off valve and one other
32
Bleed air used for?
Starting engines, cabin heating, cooling, pressurisation
33
Purpose of engine oil system?
To lubricate main bearings
34
Rpm monitored on?
Phonic wheel
35
Tachogenerator measures?
Engine speed
36
Materials should be?
High strength Low cost Light Easy to make
37
Design lidimit?
Max lod the designer would expect an airframe to experience in service
38
Wing structure
Ribs, rear spa are the 2 answers
39
Wing loading?
Loads on the wing from manoeuvre and the pay load. Payload and G is wing loading
40
Name 3 wing positions?
See pic
41
Empenade?
.
42
All flying tail plane?
Used on heavy cargo aircraft
43
Canard
A full plane and reduces drag trim at high speed
44
Tail plane on tornado?
Taileron for pitch and roll
45
V type tail plane is for
Pitch and yaw
46
Secondary flying controls?
Lateral axis elavators Normal axis Longitudinal axis
47
Horizontal stabiliser
All flying tail plane as whole angle of attack can be changed
48
Fire detection system is to
Detect fire or accessible heat
49
Areas detectors in
Cargo holds baggage areas, engines
50
Spot detectors
Anywhere that could get hot. All over the place.
51
Fire warning
Visual and audible warning
52
Problems common in what areas?
High electrical areas.
53
Fire wire?
Steel tube with inner wire. Both are charged. If the insulating material gets heated up they make the circuit
54
Fuel leaks IVO hit equipment
.
55
Correct ground de icing procedure
Clear off snow etc, then start spraying de icer
56
Identify a wing icing probe
Stick out side of a/c wing
57
Where is air taken from for anti icing?
Bleed air from the compressor.
58
Stress is?
Load per area unit of cross section
59
Strain is?
Deformation caused by stress
60
Stiffness or rigidity is?
Ratio of stress over strain.
61
Design load limit is?
Maximum load the designer would expect an airframe to experience in service.
62
High wing?
Enables ease of cargo loading
63
Mid-wing?
Low RCS
64
Low wing
Shorter undercarriage, crash protection