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Atlas / NTSB / WPR11CA486

NTSB CAROL · Event

Event WPR11CA486

2011-07-19 Brigham City, Utah, United States None 1 aircraft Status: Completed

Registry · N797V

FAA Aircraft Registry record.

Make / Model

SCHLEICHER ASW-27

Year of manufacture

2000 · 11 years old at event

Engine

NONE NONE

Seats / Engines

1 seats · 1 engine

Last airworthiness date

20010227

ADS-B equipped

Yes — Mode-S AAD3E1

Registrant of record

GIBSON CALVIN DAVID

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The glider pilot did not take timely action to locate a safe outlanding area after entering an area where atmospheric lift was not sufficient to maintain soaring flight.

Factual narrative

While participating in a soaring contest, the glider pilot entered an area where atmospheric lift was not sufficient. Instead of jettisoning the glider's water ballast to reduce its sink rate and reversing his course toward better outlanding fields, he continued on with the contest course and task. He therefore ultimately ended up in a location where he was forced to attempt an off-airport landing on unsuitable terrain. Immediately upon touchdown, the glider encountered several small boulders that were hidden in the grass, and the left wing tip became snagged in some tall grass, resulting in a loss of directional control. During the resulting ground loop, both wings sustained substantial damage and the empennage tail boom separated from the main part of the fuselage. While participating in a soaring contest, the glider pilot entered an area where atmospheric lift was not sufficient. Instead of reversing his course toward better outlanding fields, he continued with the contest course and task. He ultimately ended up in a location where he was forced to attempt an off-airport landing on unsuitable terrain. Immediately upon touchdown, the glider encountered several small boulders that were hidden in the grass, and the left wing tip became snagged in some tall grass, resulting in a loss of directional control. During the resulting ground loop, both wings sustained substantial damage and the empennage tail boom separated from the main part of the fuselage. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • Environmental issues-Physical environment-Terrain-Rough terrain-Contributed to outcome
  • Environmental issues-Physical environment-Terrain-(general)-Contributed to outcome
  • C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
  • Environmental issues-Conditions/weather/phenomena-(general)-(general)-Effect on operation

Verbatim from NTSB's published report. Source file NTSB_2011_WPR11CA486.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.