NTSB CAROL · Event
Event LAX02LA160
Aircraft involved
Probable cause & findings
The failure of the pilot to maintain sufficient airspeed during the attempted go-around resulting in a stall/mush. The gusting winds, recent purchase of airplane, and premature raising of the flaps were factors.
Factual narrative
On May 12, 2002, about 1615 Pacific daylight time, an amateur-built Mulligan RV4 airplane, N6579B, collided with the ground during an attempted go-around from runway 26 at the Santa Ynez, California, airport. The airplane was owned and operated by the pilot under the provisions of 14 CFR Part 91. The private pilot and sole passenger were not injured; the airplane sustained substantial damage. The personal local flight departed Santa Ynez airport about 1545. Day visual meteorological conditions prevailed and no flight plan had been filed. The accident was initially reported by the Santa Barbara County Fire Department, which has a station close to the Santa Ynez airport. The captain on duty at the time of the event stated that they observed the accident airplane approach runway 26 "flying nearly sideways." The firefighters at the station then lost sight of the airplane as it descended from their view. The station responded to the reported accident and secured the scene from fire ignition danger. The captain reported that the fuel tanks contained "lots of fuel." At the time of the accident he estimated that the winds were from the west about 10 mph. The captain noted that the "entire airplane" including the wings, engine compartment, firewall, and tail surfaces sustained damage. The pilot was interviewed by telephone on May 12, 2002. He reported that he had recently purchased the airplane. He was on final approach to runway 26 when a gust of wind caused the airplane to balloon up. He elected to go-around and added full power, then retracted the flaps. During this time, the airplane was drifting off the left side of the runway. The pilot stated that for "undetermined reasons" the airplane settled to the ground. The left wing contacted the ground, followed by the airplane's nose. He estimated that the winds were from 260 degrees at 10 mph, with gusts to 15 to 20 mph. The pilot said he is not aware of any mechanical problems with the airplane before the accident sequence. In a written statement received May 22, 2002, the pilot stated a gust lifted the aircraft after the tailwheel had touched down. Full throttle was applied and the aircraft proceeded slowly without gaining speed in level flight at about 25 feet agl. The speed did not increase so the pilot raised the flaps; however, the speed did not increase. The airplane was in level flight, just above ground level, with full throttle when it "apparently stalled." The amateur-built airplane collided with the ground during an attempted go-around from runway 26. The pilot reported he was on final approach when a gust of wind caused the airplane to balloon up. He elected to go-around and added full power, then retracted the flaps. During this time, the airplane was drifting off the left side of the runway. The pilot stated that the airplane "apparently stalled" and settled to the ground. The left wing contacted the ground, followed by the airplane's nose. He estimated that the winds were from 260 degrees at 10 mph, with gusts from 15 to 20 mph. The pilot stated he had recently purchased the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_LAX02LA160.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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