NTSB CAROL · Event
Event CHI91LA118
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO ATTAIN PROPER RUNWAY ALIGNMENT AND NOT MAINTAINING DIRECTIONAL CONTROL WHICH RESULTED IN A GROUND LOOP. FACTORS RELATING TO THIS ACCIDENT WERE THE GUSTY CROSSWIND CONDITIONS WHICH EXISTED AT THE TIME.
Factual narrative
THE PILOT OF A SINGLE ENGINED TAILWHEEL AIRPLANE DID NOT ATTAIN PROPER ALIGNMENT WHILE PERFORMING A CROSSWIND LANDING IN GUSTY CONDITIONS. AIRPLANE CONTROL WAS NOT MAINTAINED AND THE AIRPLANE GROUNDLOOPED, COLLAPSING THE MAIN LANDING GEAR. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_CHI91LA118.txt.
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Related research
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Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
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