Which consequence results when hydraulic check valve chatter occurs in an aircraft landing gear system?

💡 Explanation

Increased actuator component fatigue emerges because pressure fluctuations from check valve chatter induce repetitive stress cycles—a form of mechanical resonance. Therefore fatigue accelerates, rather than temperature dropping. This impact is localised to the landing gear affecting actuators more than other wings.

• In aircraft forging, which consequence results when dies are improperly aligned?
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