Narrative:

During the final two-three seconds (approximately) prior to touchdown; at an altitude of less than 50 ft. (Approximately); we encountered a loss of airspeed that momentarily triggered the stick-shaker. The approach was stable at 500 ft. AGL and; due to the conditions present; I briefed my intention to maintain an airspeed at the 'top of the bug'. At 100 ft. AGL; the pm (pilot monitoring) noted the airspeed to be at vref+10. While descending below approximately 50 ft. AGL; the airspeed decayed rapidly; until reaching approximately 120 KIAS (as reported by the pm during the post-flight de-briefing) at touchdown. [This was an approximate 15- to 20-kt loss]by my estimation; this event occurred due to two primary factors; the first of which was the challenging weather conditions at touchdown. I mitigated these threats by briefing the conditions; flying a reasonably faster airspeed; and diligently anticipating and reacting to the gains and losses of airspeed. The sudden last-second decay in airspeed was unforeseen; yet not severe enough (given present altitude and idle thrust) to warrant a go-around as a safer course of action. Secondly; the stick-shaker may have been activated through a temporary and anomalous triggering of the stall protection system. This theory was further substantiated by the fact that the very next landing (under nearly ideal circumstances; and good; smooth technique) saw an activation of the auto-ignition system at approximately 20 ft. AGL.

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Original NASA ASRS Text

Title: CRJ-200 Captain reported stick shaker during landing.

Narrative: During the final two-three seconds (approximately) prior to touchdown; at an altitude of less than 50 ft. (approximately); we encountered a loss of airspeed that momentarily triggered the stick-shaker. The approach was stable at 500 ft. AGL and; due to the conditions present; I briefed my intention to maintain an airspeed at the 'top of the bug'. At 100 ft. AGL; the PM (Pilot Monitoring) noted the airspeed to be at VREF+10. While descending below approximately 50 ft. AGL; the airspeed decayed rapidly; until reaching approximately 120 KIAS (as reported by the PM during the Post-flight De-briefing) at touchdown. [This was an approximate 15- to 20-kt loss]By my estimation; this event occurred due to two primary factors; the first of which was the challenging weather conditions at touchdown. I mitigated these threats by briefing the conditions; flying a reasonably faster airspeed; and diligently anticipating and reacting to the gains and losses of airspeed. The sudden last-second decay in airspeed was unforeseen; yet not severe enough (given present altitude and idle thrust) to warrant a go-around as a safer course of action. Secondly; the stick-shaker may have been activated through a temporary and anomalous triggering of the Stall Protection System. This theory was further substantiated by the fact that the very next landing (under nearly ideal circumstances; and good; smooth technique) saw an activation of the Auto-Ignition system at approximately 20 ft. AGL.

Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.