Chp1 Airframes Flashcards

1
Q

Name as many parts of an aircraft as possible

A

Fuselage, Wing leading edge, Wing trailng edge, Fin, Tailplane, Elevator, Rudder, Wing root, Flaps, Aileron, Wing tip, Main plane, Engine nacelle

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2
Q

Name a type of ground load exerted on an aircraft

A

weight, friction, reverse, braking, taxing, takeoff/landing, towing, hoisting cargo

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3
Q

Name a type of flight load exerted on an aircraft

A

weight, aerodynamic forces, thrust, pressurisation

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4
Q

Name the two abnormal loads that an aircraft could experience

A

Asymmetric flight
Landing on nose gear

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5
Q

What is the primary structure of an aircraft

A

The pars designed to withstand the largest stresses and if it fails, the integrity of the aircraft can be comprimised and suffer a catastrophic failure

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6
Q

What is the function of the secondary structure?

A

Also designed to withstand stress but less amounts
If catastrophic failure occurs then it could result in limitations to the operation

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7
Q

In the EASA environment what certain specifications are defined by competent authorities for the design/manufacture operation?

A

CS-25 = large aeroplanes
CS-23 = light aeroplanes

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8
Q

What is a CS comprimised of?

A

Design, material quality, build quality ect…

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9
Q

What does AMC stand for?

A

Acceptable means of compliance

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10
Q

What is the GM?

A

Guidance Material whichh is extra tips on how to follow the CS

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11
Q

What are the three types of loads?

A

Static
Dynamic
Cyclic

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12
Q

What is static load?

A

When a force is continually applied and does not change
The aircraft will be in steady level flight

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13
Q

What is dynamic load?

A

When a force continuously changes over time
When there is a change in lift due to turbulence

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14
Q

What is cyclic load?

A

When a force is continually applied and removed, reduced or reversed
When the aircraft cabin is pressurised or the load exerted on the undercarridge during landing or takeoff

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15
Q

What are the different ways a load can be applied?

A

Tension
Compression
Bending
Shear
Torsion
Or a combination

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16
Q

Define stress

A

An internal force per unit of area that occurs as a result of external loads

17
Q

Define strain

A

The ratio of the change in length against the original length

18
Q

What is the difference between elastic and plastic deformation

A

Elastic deformation is one that is seen when a load is applied then it reverts back to its orginal state compared to Plastic deformation which is permanent

19
Q

What is corrosion

A

The break down of metal through a chemical or electrochemical attack, it occurs when there are conditions to provide electrolytes

20
Q

What is surface corrosion

A

When the cross sectional thickness of the material is reduced
It can be seen as etching or pitting in the material

21
Q

what happens in the corrosion between materials

A

It occurs when two dissimilar metals are in contact, fueled by the presence of an electrolyte. It can penetrate the core of the metal along grin boundaries.
It can also be accelerated by stress

22
Q

What environments is corrosion most lkely to occur

A

When there is a high presence of salt, pollutants or chemicals and high humidity

eg. marine, tropical or industrial environments

23
Q

what are some signs or corrosion

A

discolouration
flaking
cracks
powdering
rust ect…

24
Q

What are some materials carried on aircraft that could accelerate corrosion?

A

Battery acid
Water
Toilet wastewater
Hydraulic fluids when mixed with water

25
What are some ways to minimise corrosion?
Protective paint surface treatment Washing and cleaning regularly Long term storage in dry environments