Aircraft Structural Repair & NDI Flashcards

1
Q

Procedure for penetrant inspection (4)

A

Apply penetrant
Remove excess penetrant
Apply developer
Surface indication

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2
Q

Marks penetrating the surface that reduce the cross-sectional area but do not penetrate the complete thickness of the material are known as ____?

A

scratches

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3
Q

Disbonds are areas within the bonded surface between two adherents in which _____ has occurred

A

adhesion failure or separation

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4
Q

Delamination involves the _____

A

separation of layers

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5
Q

Types of Repairs: (5)

A
Insertion - Inserting a new section and splicing it to the affected member
Replacement
Negligible
Patch
Blending / Stop-Drill Repair
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6
Q

An eddy current probe ______ with the test material to detect eddy currents

A

must be in contact

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7
Q

Magnetic particle inspections can _________

A

detect near-surface and surface defects in ferromagnetic materials.

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8
Q

Structures with temporary repairs must be ______

A

replaced or repaired at the earliest opportunity.

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9
Q

_______ permits an aircraft to fly until the opportunity to carry out a permanent repair presents itself.

A

An acceptable defect

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10
Q

What flaw can penetrant inspection detect?

A

surface flaws

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11
Q

What can ultrasonic inspection detect?

A

surface and inter-surface defects in metals and composite materials.

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12
Q

What is the best method to inspect internal and inaccessible structural parts

A

radiography

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13
Q

What is used for visual inspection?

A

Borescopes [Boroscopes]

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14
Q

How are cracks formed?

A

Exposure to a corrosive environment while subjected to sustained tensile stress are known as stress corrosion cracks.

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