NTSB CAROL · Event
Event LAX97LA318
Aircraft involved
Probable cause & findings
the student pilot's improper recovery from a bounced landing, and failure to maintain adequate airspeed during an attempted go-around, which resulted in a stall and impact with the terrain (runway).
Factual narrative
On September 8, 1997, at 1030 hours mountain standard time, a Beech A23A, N2339W, bounced into the air and subsequently drug the left wing on the runway after an unsuccessful go-around attempt at La Cholla Airpark, Tucson, Arizona. The aircraft was destroyed during the impact sequence, and the student pilot was not injured. The flight originated at La Cholla Airpark at an undetermined time. Visual meteorological conditions prevailed at the time of the accident. The flight was the first solo cross-country flight for the student pilot. The intended route of flight was La Cholla, Bisbee, Wilcox, and then back to La Cholla. The student pilot was interviewed by an FAA Operations Inspector on September 10, 1997. The inspector stated that the pilot reported that the stall warning horn came on before he touched down on the runway. The student pilot said he touched down about 30 feet past the "numbers" on the runway. After landing, the airplane bounced into the air about 10 feet. The student pilot said he realized that the aircraft was too slow and added full power to execute a go-around. He estimated that he was approximately 10 to 20 feet in the air when the stall warning horn went off again. The aircraft banked to the left and descended with the left wing hitting the ground first. The airplane went off the left side of runway 19. The student pilot said he did not believe that there were any mechanical malfunctions that may have contributed to the accident. The student pilot was returning to the originating airport from his first solo cross-country flight. He reported that the stall warning horn came on before the airplane touched down, about 30 feet past the numbers, then the plane bounced into the air about 10 feet. The student said he realized that the airplane was at too slow an airspeed, and he attempted to execute a go-around by adding full power. The airplane climbed to approximately 20 feet in the air, then the stall warning horn sounded again. The airplane then banked to the left and impacted the ground. The student said he did not believe that there were any mechanical malfunctions that may have contributed to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_LAX97LA318.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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