NTSB CAROL · Event
Event LAX06CA223
Aircraft involved
Probable cause & findings
the pilot's failure to maintain an adequate airspeed during a go-around, which resulted in a stall/mush. A contributing factor was the high density altitude.
Factual narrative
On July 3, 2006, about 1140 Pacific daylight time, a Piper PA-28-181, N6413C, collided with terrain during an attempted go-around at Butte Valley Airport, Dorris, California. Tradewinds Aviation was operating the airplane under the provisions of 14 CFR Part 91. The renter private pilot and three passengers were not injured; the airplane sustained substantial damage. The local personal flight departed Butte Valley about 1030. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot submitted a written report. On the morning of the flight, the pilot calculated the weight and balance limitations, density altitude, and checked the weather forecast for the area using the Automated Digital Data System (ADDS). The flight departed Butte Valley Airport at 1030, and returned 1 hour later. The pilot circled over the airport and determined that the winds were calm. He entered a left traffic pattern for runway 34 and extended his downwind leg to properly set up for the approach. Upon turning final, the airplane was configured with 40 degrees of flaps. The pilot noticed a slight crosswind from the west and applied crosswind correction. On short final, the airplane was aligned with the runway with an indicated airspeed of about 65 knots. The airplane crossed the approach end of the runway 50 feet above ground level (agl). At this time, the airplane rolled suddenly to the left and the stall warning horn briefly sounded. The pilot initiated a go-around by applying full power and retracting the flaps to 25 degrees. The pilot attempted to correct the airplane's left turning tendency with right rudder input. As the airplane continued to descend, the pilot released right rudder pressure and leveled the wings in an attempt to climb. The airplane continued to descend on a heading of 310 degrees. About 10 feet agl, the pilot pulled back on the yoke in an effort to slow the airplane down as much as possible. The airplane touched down on the main landing gear in a field about 100 yards west of the runway. The left wing dug into the ground and the airplane spun 90 degrees to the left before coming to a stop. Butte Valley Airport is located at an elevation of 4,243 feet. At the time of the accident, the Klamath Falls Airport Automated Surface Observing System, 20 nautical miles northeast of the accident site, reported a temperature of 26 degrees Celsius and a barometric pressure of 30.13 inches of Mercury. The calculated density altitude for Butte Valley Airport using Klamath Falls weather information at the time of the accident was 6,313 feet. The airplane impacted the ground during an attempted go-around. Before the flight, the pilot performed weight and balance and density altitude calculations. After a 1-hour local flight, the pilot circled over the airport and determined the winds to be calm. He entered the traffic pattern for runway 34 and extended 40 degrees of flaps. The pilot noticed a slight crosswind from the west and applied crosswind correction. On short final, the airplane was aligned with the runway at an indicated airspeed of 65 knots. As the airplane crossed the approach end of the runway it rolled to the left and the stall warning horn sounded. The pilot initiated a go-around by applying full power and retracting the flaps to 25 degrees. The airplane continued to descend, so the pilot released right rudder pressure and leveled the wings in an attempt to climb; however, the airplane continued to descend on a heading of 310 degrees. About 10 feet above ground level, the pilot pulled back on the yoke in an effort to slow the airplane down. The plane touched down on the main landing gear in a field about 100 yards west of the runway. The left wing dug into the ground and the airplane spun 90 degrees to the left before coming to a stop. The calculated density altitude was 6,313 feet. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_LAX06CA223.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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