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Atlas / NTSB / LAX96LA060

NTSB CAROL · Event

Event LAX96LA060

1995-12-01 ADELANTO, California, United States Airport · 0CL1 Serious 1 aircraft Status: Completed

Registry · N6LS

FAA Aircraft Registry record.

Make / Model

BEECH E-55

Year of manufacture

1981 · 14 years old at event

Seats / Engines

6 seats · 2 engines

Last airworthiness date

19801219

ADS-B equipped

Yes — Mode-S A7C398

Registrant of record

9 SECONDS CONSULTING LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the pilot's selection of the wrong runway for the prevailing wind conditions, and his failure to maintain an adequate airspeed during the base-to-final turn.

Factual narrative

On December 1, 1995, at 1418 hours Pacific standard time, a Laister Sailplane LP-15, N6LS, collided with the ground during the base-to-final turn while landing at Krey Field, Adelanto, California. The glider was operated as a personal flight when the accident occurred. The glider was destroyed and the certificated private pilot was seriously injured. Visual meteorological conditions prevailed. Witnesses reported the pilot was towed toward the east to an altitude of 3,000 feet above ground level (agl), and the weather conditions at the time of landing favored a landing to the west. The glider was observed on a downwind leg of the traffic pattern heading west into the wind. An FAA designated pilot examiner for gliders witnessed the accident. The speed and altitude of the glider was reported as slow and low. During the base-to-final turn for runway 09 about 50-75 feet agl, the left wing of the glider was observed to drop. The witness said the glider appeared to stall and then descend to ground impact. Examination of the glider by the airport manager after the accident did not reveal any evidence of mechanical failure or malfunction. The field is equipped with three windsocks. According to witnesses, the windsocks were indicating a wind from the west at 10-12 knots at the time of the accident. THE PILOT ENTERED THE AIRSTRIP TRAFFIC PATTERN AND SET UP FOR A DOWNWIND FINAL APPROACH TO RUNWAY 9. THE WINDSOCKS WERE INDICATING A WIND FROM THE WEST AT 10-12 KNOTS AND FAVORED A LANDING TO THE WEST. AN FAA DESIGNATED PILOT EXAMINER FOR GLIDERS WITNESSED THE ACCIDENT AND REPORTED THAT THE SPEED AND ALTITUDE OF THE GLIDER WAS SLOW AND LOW. THE GLIDER BEGAN A BASE-TO-FINAL TURN ABOUT 50-75 FEET AGL AND THE LEFT WING OF THE GLIDER DROPPED. THE EXAMINER SAID THE GLIDER APPEARED TO STALL AND THEN DESCEND TO GROUND IMPACT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_LAX96LA060.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 or causal vocabulary (stall). 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 ↗