Day 3 Progress Check Flashcards

1
Q

What distinguishes the monocoque structure from the semimonocoque in terms of load-bearing?

A

Semimonocoque uses both skin and internal framework to support loads.

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2
Q

How is a surface repair patch typically installed on aircraft skin?

A

By installing a patch over the external surface, often called a scab patch.

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3
Q

In aircraft surface repairs, how is the dimension of a chamfer typically determined?

A

3 to 4 times the material thickness from the edge into the surface.

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4
Q

What is one key element of aircraft wings as described in the SRM?

A

Wings typically have at least two spars, front and rear.

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5
Q

What are longerons primarily responsible for in an aircraft’s structure?

A

Providing structural integrity against twisting and bearing tension.

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6
Q

What is the primary function of stringers in aircraft structural design?

A

To prevent twisting and manage tension, similar to longerons but lighter.

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7
Q

According to the Basic Sheet Metal Structural Repair Manual, what type of patch should be designed for a crack repair?

A

A repair patch double the size of the damaged area.

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8
Q

Which of the following is NOT a chapter covered under the ATA Codes’ Aircraft Structures?

A

Chapter 60 Control Surfaces

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9
Q

What is the main difference in the classification between primary and secondary aircraft structures?

A

Primary structures are essential for flight; secondary structures are not.

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10
Q

What type of wings relies entirely on the wing’s own structure for support?

A

Cantilever Wings

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11
Q

Which chapter of the ATA Codes focuses specifically on wing repairs and maintenance?

A

Chapter 57 Wings

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12
Q

What is the purpose of using ATA Codes in aircraft maintenance documentation?

A

To standardize the filing and retrieval of commercial aircraft information.

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13
Q

In the context of the SRM, what is the role of gussets?

A

To join and reinforce structural members like frames and stringers.

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14
Q

How should repairs be executed if the aircraft has a Structural Repair Manual (SRM)?

A

In compliance with the SRM or applicable Engineering Orders, no exceptions.

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15
Q

Which ATA chapter deals specifically with the fuselage?

A

Chapter 53 Fuselage

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