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Which hazardous cascade initiates if aircraft landing gear fails to fully deploy?

A)Asymmetric lift-induced rolling moment
B)Loss of altimeter calibration settings
C)Hypergolic fuel ignition anomaly
D)Catastrophic sensor data synchronization

💡 Explanation

Partial gear extension alters wing airflow triggering **unequal lift distribution**, because one side creates significantly more drag than the other; therefore unstable rolling results, rather than altimeter errors or fuel malfunctions which are independent systems.

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