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Which outcome results when the trim control system inadequately compensates for changes in an aircraft's center of gravity during flight?

A)Increased pilot workload and fatigue
B)Decreased fuel efficiency marginally
C)Complete structural disintegration occurs later
D)Elevated cabin pressure subtly increases

💡 Explanation

Increased pilot workload occurs because aerodynamic forces induce unwanted pitch or roll; therefore the pilot must constantly exert force to maintain intended flight, rather than allowing the trim tab to stabilize the aircraft. Other outcomes are less direct given a functioning aircraft.

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