Which risk increases when aircraft landing gear experiences strut over-compression?

💡 Explanation

Increased fuselage skin fatigue cracking is the greatest risk because strut over-compression transfers excessive stress directly to the airframe via *stress concentration*, therefore fatigue cycles accumulate faster, rather than affecting braking or engine functions.

• Which outcome occurs when cryogenic pump experiences sustained cavitation?
• Which consequence results when exceeding the slenderness ratio limit in supporting columns?
• Which consequence results when excessively rapid switching occurs in induction motor drives?
• Which instability occurs when thrust reversers are deployed late during landing?
• Which risk increases when reactive var compensation inadequately corrects transmission-line voltage sags during heavy inductive loading of an electrical grid?
• Which outcome occurs when a solid-state relay driving an inductive load experiences voltage overshoot?