Which consequences results when an aircraft's flight controls experience single-point actuator failure during flight?

💡 Explanation

Flight control failure leads to uncommanded surface deflection because hydraulic lock causes uncontrolled movement exceeding limits, therefore leading to abrupt pitch change, rather than fatigue, communication failures because these functionalities are distinct.

• Within substation transformers undergoing high reactive power load fluctuations, which outcome occurs when tap-changer inertia prevents rapid voltage adjustments?
• Which risk increases when wing-mounted spoilers fail to deploy during descent?
• Which risk increases significantly when over-sensitizing ground fault circuit breakers (GFCI)?
• Which outcome occurs when a power transformer with solid-state circuit breakers experiences sustained inrush current after energization?
• Which condition occurs in a diesel engine when lubricating oil enters the combustion chamber?
• Which risk increases when a hydraulic directional control valve experiences spool binding in a high-pressure system?