NTSB CAROL · Event
Event FTW98LA244
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 ↗.
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