Which risk increases when an aircraft's flight-spoiler doors activate asymmetrically?

💡 Explanation

Flight-spoiler asymmetry causes differential lift force, triggering **adverse yaw,** because unequal drag induces a rolling moment. Therefore, the risk is uncontrolled roll, rather than solely increased drag or loss of efficiency which could occur symmetrically under controlled deployments.

• Which outcome occurs when a refrigeration system uses an immiscible refrigerant blend circulating at low temperatures?
• Which risk increases when a hydraulic actuator drives an oscillating load near its resonant frequency?
• Which outcome occurs when viscous boundary layer separation becomes significant around an aircraft's landing gear during descent?
• Which undesirable consequence arises when dispersion becomes excessive in single-mode fiber optic data transmission?
• Which outcome will occur in an aircraft if the stability augmentation system (SAS) actuators exceed their maximum rate limits?
• Which effect limits the performance of an axial flow pump in a cryogenic refrigeration system?