The Airframe Flashcards

1
Q

What material usually forms the skin of an aircraft?

A

Aluminium

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2
Q

The fuselage is of what kind of construction?

A

Semi-monocoque

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3
Q

What is a monocoque construction?

A

No internal structure
Stress carried by the skin

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4
Q

What is a strut-type construction?

A

Internal framework carries all the stress

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5
Q

Semi-monocoque construction is a compromise between what two types?

A

Strut-type and monocoque

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6
Q

The windscreen typically consists of what material?

A

Perspex

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7
Q

Properties of perspex?

A

Easily scratched

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8
Q

In a wing, what attaches to the fuselage and extends to the wing tip?

A

Spar

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9
Q

What carries the major loads in a wing?

A

Spars

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10
Q

What wing structure provides external strength by transmitting extra loads to the fuselage?

A

Struts

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11
Q

What does a strut do?

A

Transmits extra loads of the fuselage

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12
Q

What structures run roughly perpendicular to the spars? in a wing

A

Ribs

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13
Q

What do ribs transmit?

A

Loads between the skin and the spars

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14
Q

What transmits loads between skins and spars?

A

Ribs

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15
Q

What calculation identifies the physical loads that an aircraft will undergo?

A

Stress analysis

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16
Q

What is stress caused by?

A

External forces acting on a material

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17
Q

What is stress?

A

Internal force that opposes deformation

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18
Q

What is strain?

A

The degree by which a material has been defroemd from a force or load

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19
Q

How are stress and strain different?

A

Stress is resistance to deformation
Strain is the degree of deformation

20
Q

What are the 5 major stresses?

A

Compression
Tension
Shear
Torsion
Bending

21
Q

What is tension?

A

Pulling apart

22
Q

What is compression?

A

Pushing together

23
Q

What is torsion?

A

Twisting apart

24
Q

What is shear?

A

Laterally shifting layers about a point

25
Q

What occurs at the outside of a bend?

26
Q

What occurs at the inside of a bend?

A

Compression

27
Q

What stresses are aircraft meant to avoid?

28
Q

Instead of bending, what are aircraft parts meant to undergo?

A

Tension and compression

29
Q

Why is nylon better than manila rope (for tying down aircraft)?

A

It is more elastic and less likely to shrink when wet

30
Q

How does carbon monoxide affect the body?

A

Displaces oxygen from the bloodstream

31
Q

What can be fitted to the flight control system to prevent excessive movement?

32
Q

The flight control system on most light training aircraft are of what type?

A

Mechanical flight control system

33
Q

What is the Elastic Limit?

A

The limit of distortion at which the structure returns to its original shape and dimensions

34
Q

What is the limit of distortion at which the structure returns to its original shape and dimensions?

A

Elastic limit

35
Q

What is the Yield Point?

A

The point at which deformations become permanent

36
Q

What is the point at which deformations become permanent

A

Yield Point

37
Q

What is the Ultimate Load?

A

The load at which failure of the structure occurs

38
Q

What is the load at which failure of the structure occurs?

A

Ultimate Load

39
Q

What does Fail Safe mean?

A

If one part fails, the remaining parts in the system will continue to operate

40
Q

What does Safe Life mean?

A

A component is released with a specific ‘life’ of hours or cycles, until replacement

41
Q

If one part fails, the remaining parts in the system will continue to operate. This is given what term?

42
Q

A component is released with a specific ‘life’ of hours or cycles, until replacement. This is given what term?

43
Q

The main weight of the aircraft is supported by what structures?

A

The main spar, connected to the undercarriage

44
Q

What are fuselage formers?

A

Components that provide only ‘shape’ to the fuselage