Which undesired effect occurs when a helicopter's cyclic control aggressively commands forward flight?

💡 Explanation

Dynamic roll-over is a risk because the differential lift causes sideways thrust while landing gear friction prevents lateral movement, therefore the helicopter rolls, rather than translating as intended; compressibility stall affects high speed flight.

• Within a three-phase power transformer, which consequence results when an inductive load causes a leading power factor correction circuit to switch inappropriately?
• Which outcome occurs when fuel injectors in a modern diesel engine experience prolonged dribbling due to wear?
• Which consequence results when a retractable aircraft landing gear system experiences hydraulic pump cavitation?
• Which risk is heightened when post-tensioned concrete beam tendons experience unexpected slippage during anchoring?
• Which outcome occurs within a liquid-ring vacuum pump when excessive gas dissolved within it cavitates?
• Which risk increases when a hydraulic actuator on an aircraft landing gear experiences rapid, repeated cycling?