Which system impairment develops when an aircraft's fly-by-wire system experiences latency exceeding sensor feedback sampling rate?

💡 Explanation

When latency exceeds the sampling rate, the control system becomes unstable because feedback signals are out of sync with actual aircraft dynamics, leading to oscillations as the system overcorrects. Therefore control surface oscillation results, rather than engine flameout, navigation drift, or hydraulic issues, which require separate malfunctions.

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