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Atlas / NTSB / FTW98LA414

NTSB CAROL · Event

Event FTW98LA414

1998-08-31 SHERMAN, Texas, United States Airport · F39 None 1 aircraft Status: Completed

Aircraft involved

Probable cause & findings

The failure of the pilot in command to maintain directional control of the airplane during the landing flare. A factor was the gusty, crosswind condition.

Factual narrative

On August 31, 1998, at 1800 central daylight time, a Pitts S-2B tail wheel equipped airplane, N52TW, was substantially damaged following a loss of control while landing at the Grayson County Airport, near, Sherman, Texas. The private pilot, owner and operator of the airplane, and sole occupant, was not injured. Visual meteorological conditions prevailed for the Title 14 CFR Part 91 local personal flight that originated from the Grayson County Airport at 1700. A flight plan was not filed. The pilot stated in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that he entered the downwind leg for landing on runway 17L and noticed that the windsock indicated an "80 to 90 degree crosswind." Just prior to the wheels of the airplane contacting the runway "a gust of wind from 090 degrees" pushed the bi-plane to the right of the runway centerline. The airplane contacted the runway to the right of the runway centerline. The pilot tried to maintain directional control by "applying left rudder and brakes." Subsequently, the tail of the airplane started to swing out to the right and the right main gear collapsed. The airplane slid approximately 15 feet before stopping upright on the runway. The pilot estimated that at the time of the accident, the wind was from 090 degrees at 10 to 12 knots, gusting to 15 knots. The pilot had accumulated a total of 122 hours in the make and model. The airplane had accumulated a total of 112 hours since new. An FAA inspector examined the airplane after the accident and stated that the right main gear collapsed and the lower right wing was structurally damaged. The pilot added that the right wing sustained spar and rib damage. The pilot of the tail wheel equipped airplane lost directional control while landing on runway 17L due to a crosswind condition. The private pilot stated that just prior to the wheels contacting the runway a gust of wind 'from 090 degrees' pushed the airplane to the right of the runway centerline. The airplane contacted the runway to the right of the runway centerline and the pilot began to use left rudder and braking to maintain directional control of the airplane. Subsequently, the tail of the airplane began to swing around to the right and the right main landing gear collapsed. The airplane slid approximately 15 feet and came to rest upright on the runway. The pilot estimates that at the time of the accident the winds were from 090 degrees at 10 to 12 knots and gusting to 15 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_FTW98LA414.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗