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.

• Which risk increases when a control valve in a chemical reactor feed line cycles too rapidly?
• Within PLC-controlled robotic arms, which consequence results from encoder signal aliasing?
• Which outcome occurs when harmonics circulate in transformer windings?
• Which outcome occurs when hydraulic actuator internal seals degrade within a robotic arm joint?
• Which fault arises when checksum errors corrupt PLC ladder logic?
• Which limitation arises when excessively increasing stray capacitance within a resonant power converter circuit?