Which mechanism causes stick-shaker activation during powered flight near stall?

💡 Explanation

Stick-shaker activates due to angle-of-attack sensor malfunction driving erroneous stall warnings, not control surface limits. This erroneous signaling triggers stall warning systems, therefore the stick shaker operates inappropriately, rather than activated due to surface saturation or instability.

• Which risk increases when an electrohydraulic actuator supporting a wind turbine blade experiences high-frequency vibrational loading?
• Which mechanical consequence results when a crankshaft experiences torsional resonance in an internal combustion engine?
• Which outcome occurs when mismatched impedance connects transceivers to antennae?
• Which mechanism primarily enhances LED efficiency in microdisplays?
• Which risk increases when progressive die stamping exceeds tolerance limits due to thermal expansion?
• Which risk increases when a hydraulic actuator's cylinder walls thin?