NTSB CAROL · Event
Event LAX95LA275
Aircraft involved
Probable cause & findings
the failure of the pilot to maintain airspeed in a turn during high wind conditions while executing a go-around at a low altitude, which resulted in an inadvertent stall and an uncontrolled descent into the ground.
Factual narrative
On July 29, 1995, at 1527 hours Pacific daylight time, a Beech P35, N9599Y, owned and operated by the pilot, crashed during a go-around at the airport in Elko, Nevada. The aircraft was destroyed and the private pilot was fatally injured. The aircraft had departed earlier from Ogden, Utah, with a destination of Sacramento, California. The pilot received a weather briefing from the Flight Service Station (FSS) at Cedar City, Utah, and an updated briefing from the Reno FSS for the Sacramento area when approaching Elko. According to the Elko air traffic controller, the pilot reported that he was northeast of the airport and would like to land. The winds at the time were variable from 190 to 230 degrees at 23 knots, gusting to 35 knots. The aircraft appeared to land too long and the pilot stated he was going around and would attempt to land on runway 30. The pilot made a left turn and was then observed to nose down into the ground. The pilot indicated no mechanical problems with the aircraft during these radio transmissions. According to ground witnesses, the aircraft started a left turn at a low altitude and was observed to be flying at a slow speed with the wings rocking back and forth. All of the witnesses commented on the windy conditions, with several stating the pilot was in obvious trouble because of them. It was during the turn to the left that some of them observed the aircraft stall and descend nose down into the ground. Examination of the aircraft under the supervision of an FAA inspector from the Reno, Nevada, Flight Standards District Office found that the landing gear and the flaps were retracted at the time of impact. There was no ground fire and no evidence found of an aircraft malfunction. See the attachments to this report for details. The elevation of the Elko airport is 5,135 feet and the temperature was recorded as 89 degrees. The density altitude was estimated to be about 8,000 feet. Also recorded shortly after the accident was a visibility of 2.5 miles with blowing dust and variable winds from 190 to 260 degrees at 28 knots, gusting to 38 knots. According to the tower controller, runway 05/23 was closed for construction and this was acknowledged by the pilot. The toxicological report on the pilot was negative for carbon monoxide, drugs, cyanide, and ethanol. THE CROSS-COUNTRY PILOT WAS CLEARED TO LAND ON RUNWAY 12, WITH THE WINDS REPORTED TO BE FROM 190 TO 230 DEGREES AT 35 KNOTS. THE PILOT WAS OBSERVED TO BE LANDING TOO LONG AND HE STATED HE WAS GOING AROUND. GROUND WITNESSES OBSERVED THE AIRCRAFT BEGIN A TURN TO THE LEFT, FLYING AT A SLOW AIRSPEED AND AT A LOW ALTITUDE, WITH THE WINGS ROCKING BACK AND FORTH. THEY THEN SAW THE AIRCRAFT STALL AND DESCEND NOSE FIRST INTO THE GROUND. THE OTHER RUNWAY (05/23) THAT WAS MORE FAVORABLE FOR THE WIND CONDITIONS WAS CLOSED DUE TO CONSTRUCTION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX95LA275.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
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