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Which risk increases adjacent to aircraft surface scratches because?

A)Crack propagation via stress concentration
B)Galvanic corrosion accelerates degradation slowly
C)Increased surface area oxidation reactions
D)Material fatigue due to applied tension

💡 Explanation

Crack propagation risk increases due to *stress concentration*. Existing scratches create points where stress intensifies during flight. This overcomes fracture toughness because the crack-tip stress exceeds the material threshold for breaking atomic bonds, therefore crack extends rather than blunting.

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