Day 6 Outside Work: Aircraft Structures Flashcards

1
Q

What is the primary advantage of integrating advanced composites into the aircraft structure?

A

They reduce the aircraft’s weight significantly.

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2
Q

How does the fuselage of pressurized aircraft manage stress from pressurization and depressurization cycles?

A

It is designed to resist metal fatigue and cracking.

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3
Q

How does the semimonocoque fuselage achieve its strength?

A

Through a combination of skin and internal structure to distribute loads.

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4
Q

What maintenance documentation is required for large aircraft?

A

Volumes of maintenance documentation detailing thousands of procedures.

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5
Q

How does variable geometry or ‘swing-wing’ design benefit an aircraft?

A

It allows the aircraft to adjust wing configuration in flight.

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6
Q

What role does the corrugated sheet play in wing construction?

A

It helps the wing better carry tension and compression loads.

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7
Q

How does a turboshaft engine primarily differ from a turbojet?

A

It uses most of the energy to drive a turbine rather than producing thrust.

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8
Q

What is the significance of the Type Certificate Data Sheet (TCDS) in aircraft maintenance?

A

It contains critical information about the aircraft.

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9
Q

What is the function of wing spars in aircraft design?

A

To serve as the principal structural members of the wing.

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10
Q

What is a stressed-skin design in aircraft construction?

A

The skin is designed to carry part of the flight and ground loads.

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11
Q

What does ‘semimonocoque’ imply about the aircraft’s construction?

A

The structure relies largely on its skin to support loads.

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12
Q

Why might a fuel-carrying bladder or tank be used in an aircraft wing?

A

To store fuel efficiently within the structure.

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13
Q

What is the benefit of using a truss structure in aircraft design?

A

It provides a rigid structure that can support more weight.

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14
Q

What design feature allows for higher speeds in modern aircraft?

A

Lighter, more aerodynamic fuselage designs.

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15
Q

Why are hydraulic systems widely used in aircraft controls?

A

They provide a more responsive control system.

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16
Q

How do manufacturers ensure the durability of the aircraft skin against environmental challenges?

A

By applying specialized protective coatings.

17
Q

Why is the design of access and inspection panels important in aircraft maintenance?

A

To allow for easy access to inspect and service various components.

18
Q

What is the purpose of slats in aircraft wing design?

A

To allow the wing to generate more lift at slower speeds.

19
Q

What are chip detectors in helicopter transmissions used for?

A

To alert pilots of potential internal problems.

20
Q

What is the main purpose of stringers in aircraft fuselage construction?

A

To provide additional longitudinal support and distribute load.

21
Q

What is a primary characteristic of a honeycomb panel in aircraft structures?

A

It is lightweight and has high strength.

22
Q

Which type of wing construction is often used in air transport category aircraft due to its ability to handle tension and compression loads effectively?

A

Box beam wing construction.

23
Q

Why are wing tips on some aircraft equipped with a Lucite rod?

A

To transmit light to the leading edge to indicate operational lights.

24
Q

What type of materials is typically used for the skin of high-speed aircraft to manage increased wing loading?

A

Chemically milled aluminum.

25
Q

Why is the pressurization of the aircraft cabin crucial at high altitudes?

A

To ensure adequate oxygen levels for passengers.