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Atlas / NTSB / FTW94LA197

NTSB CAROL · Event

Event FTW94LA197

1994-06-05 WELLINGTON, Colorado, United States None 1 aircraft Status: Completed

Registry · N3992

FAA Aircraft Registry record.

Make / Model

GLASFLUGEL STANDARD LIBELLE

Year of manufacture

1971 · 23 years old at event

Engine

NONE NONE

Seats / Engines

1 seats · 1 engine

Last airworthiness date

19710713

ADS-B equipped

Yes — Mode-S A4A6D6

Registrant of record

BIRD JOHN J

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

WAS THE PILOT'S IMPROPER COMPENSATION FOR THE CROSSWIND. A FACTOR WAS THE CROSSWIND.

Factual narrative

On June 5, 1994, approximately 1330 mountain daylight time, a Glasflugel Standard Libelle, N3992, was substantially damaged during landing at Wellington, Colorado. The private pilot was not injured. Visual meteorological conditions prevailed. The following is based on the pilot/operator report. The glider was towed aloft and released 2,000 feet above the ground. The pilot said that although it was his intention to capture a thermal and climb to a higher altitude, he encountered "strong sink" instead and he decided to return to the gliderport. He entered the traffic pattern at low altitude and when he turned onto the base leg, he realized he would be unable to clear obstacles between him and the runway. The pilot said he attempted to turn into the wind but did not have sufficient altitude, and the glider landed in a field "with a strong right side drift." When the tail wheel contacted the ground, the "side motion" caused the tail boom to separate. THE GLIDER WAS TOWED ALOFT AND RELEASED AT 2,000 FEET AGL. THE PILOT SAID HE ENCOUNTERED 'STRONG SINK' AND DECIDED TO RETURN TO THE GLIDERPORT. HE ENTERED THE TRAFFIC PATTERN AT LOW ALTITUDE AND WHEN HE TURNED ONTO THE BASE LEG, HE REALIZED HE WOULD BE UNABLE TO CLEAR OBSTACLES BETWEEN HIM AND THE RUNWAY. THE PILOT ATTEMPTED TO TURN INTO THE WIND BUT DID NOT HAVE SUFFICIENT ALTITUDE, AND THE GLIDER LANDED IN A FIELD 'WITH A STRONG RIGHT SIDE DRIFT.' WHEN THE TAIL WHEEL CONTACTED THE GROUND, THE 'SIDE MOTION' CAUSED THE TAIL BOOM TO SEPARATE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1994_FTW94LA197.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.