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Atlas / NTSB / FTW98LA244

NTSB CAROL · Event

Event FTW98LA244

1998-05-23 BRIGGS, Texas, United States Airport · TX23 None 1 aircraft Status: Completed

Registry · N427BG

FAA Aircraft Registry record.

Make / Model

BURKHART GROB FLUGZEUGBAU G103 TWIN ASTIR

Year of manufacture

1982 · 16 years old at event

Engine

NONE NONE

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19821103

ADS-B equipped

Yes — Mode-S A515C0

Registrant of record

ALBUQUERQUE SOARING CLUB INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's misjudgment of the distance and altitude. Factors were the lack of thermal lift and his diverted attention while on downwind.

Factual narrative

On May 23, 1998, at 1518 central daylight time, a Grob 103 glider, N427BG, was substantially damaged when it undershot the runway while landing near Briggs, Texas. The private pilot and his passenger were not injured. The glider was owned and operated by Fault Line Flyers, Inc., of Round Rock, Texas, under Title 14 CFR Part 91. Visual meteorological conditions prevailed throughout the area for the local flight for which a flight plan was not filed. The flight originated from the Fault Line Flyers Gliderport (TX23) near Briggs, Texas, approximately 10 minutes prior to the accident. According to the pilot, he released the glider from the tow plane prematurely at 1,500 feet MSL due to conflicting traffic. After "thermalling with another glider for a while, he could not find much lift," so he headed back to the airport to land. The pilot added that he was too low when he entered the downwind leg for runway 16; however, he estimated that he would be able to reach the approach end of the runway. In a written statement submitted by the pilot, he stated that he became distracted by a yellow glider that he thought was blocking the runway. The pilot reported that while maneuvering to land at the threshold for the 4,500 foot turf runway, he turned the aircraft on to the base leg prematurely; consequently, the left wing impacted the ground nearly perpendicular to the runway near the threshold. Subsequently, the glider impacted the ground in a nose low attitude, bounced back in the air and impacted the ground in a tail low attitude, separating the tail section from the airframe. Examination of the aircraft by the FAA inspector confirmed that the left wing and the tail section of the 1982 model glider sustained structural damage. The glider pilot had released the glider from the tow plane prematurely at 1,500 feet MSL due to conflicting traffic. After 'thermalling with another glider for a while, he could not find much lift,' so he headed back to the airport to land. The pilot added that he was too low when he entered the downwind leg for runway 16; however, he estimated that he would be able to reach the approach end of the runway. In a written statement, he stated that he became distracted by a yellow glider that he thought was blocking the landing runway. The pilot reported that while maneuvering to land at the threshold for the 4,500-foot turf runway, he turned the aircraft onto the base leg prematurely; consequently the left wing impacted the ground nearly perpendicular to the runway near the threshold. Subsequently, the glider impacted the ground in a nose low attitude, bounced back in the air and impacted the ground in a tail low attitude, separating the tail section. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_FTW98LA244.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. 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 ↗