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Which risk significantly increases when exceeding an airplane turbine engine's redline temperature?

A)Accelerated blade creep initiates
B)Volumetric locking reduces compression
C)Increased shaft torsion vibration exists
D)Cooling fluid vaporisation accelerates

💡 Explanation

Exceeding redline temperature causes accelerated blade creep because thermally-activated dislocation glide allows plastic deformation; the turbine blades elongate permanently. Therefore blade failure risk increases, rather than fluid vaporization, which happens at lower temperature.

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