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Atlas / NTSB / SEA94LA078

NTSB CAROL · Event

Event SEA94LA078

1994-03-08 HEBER CITY, Utah, United States Airport · 36U None 1 aircraft Status: Completed

Registry · N5790S

FAA Aircraft Registry record.

Make / Model

SCHWEIZER SGS 2-33A

Year of manufacture

1968 · 26 years old at event

Engine

NONE NONE

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19680711

ADS-B equipped

Yes — Mode-S A77241

Registrant of record

LAKE ELSINORE SOARING CLUB

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

THE FLIGHT INSTRUCTOR'S DELAYED/INADEQUATE REMEDIAL ACTION. FACTORS INCLUDE THE STUDENT PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL, AND UNFAVORABLE/VARIABLE, GUSTY WINDS DURING THE TAKEOFF ROLL.

Factual narrative

On March 8, 1994, approximately 1500 mountain standard time (MST), a Schweizer 2-33A glider, N5790S, collided with taxiway markers during the takeoff roll at Heber Valley Airport, Heber City, Utah. The certified flight instructor and his dual student were not injured, but the aircraft sustained substantial damage. The dual student, who was attempting a takeoff for a local instructional flight, was operating in visual meteorological conditions at the time of the accident. No flight plan had been filed, and there was no report of an ELT activation. According to the flight instructor, the student pilot was making the takeoff with the assistance of a wing-runner. After the flight controls became effective, the wing-runner let go of the wing. Soon thereafter, the glider veered left, and the left wing dipped sharply. The flight instructor took control of the aircraft, but his remedial action was not sufficient to keep the aircraft from departing the side of the runway and striking a runway marker. The instructor pilot aborted the takeoff by releasing the tow line after the impact with the marker. In an interview with investigators, the instructor pilot said that he believed a variable crosswind switched to a quartering tailwind during the takeoff roll, resulting in a loss of flight control effectiveness. WHILE BEING TOWED DURING A TAKEOFF ROLL, THE DUAL GLIDER STUDENT WAS NOT ABLE TO MAINTAIN DIRECTIONAL CONTROL. THE INSTRUCTOR PILOT TOOK CONTROL OF THE AIRCRAFT, AND ELECTED TO CONTINUE THE TAKEOFF. HIS REMEDIAL ACTIONS WERE INADEQUATE TO KEEP THE AIRCRAFT FROM DEPARTING THE RUNWAY, AND HE DID NOT INITIATE AN ABORT UNTIL AFTER THE GLIDER STRUCK A TAXIWAY MARKER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1994_SEA94LA078.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.