NTSB CAROL · Event
Event LAX05CA001
Registry · N4835F
FAA Aircraft Registry record.
Make / Model
CESSNA TU206A
Engine
CONT MOTOR GTSIO-520-C (340 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19660308
ADS-B equipped
Yes — Mode-S A5F6CB
Registrant of record
HERNANDEZ CHRISTOPHER A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to remain on the designated taxiway surface, which resulted in the airplane's collision with the ditch. The dark lighting condition was a factor to the accident.
Factual narrative
On October 1, 2004, at 2130 mountain standard time, a Cessna TU206A, N4835F, collided with a ditch during taxi following a landing on runway 03 at the Nogales International Airport, Nogales, Arizona. The airplane sustained substantial damage. The pilot, also the registered owner, was operating the airplane under the provisions of 14 CFR Part 91. The commercial pilot, the sole occupant, was not injured. Night visual meteorological conditions prevailed for the flight, and no flight plan had been filed. The airplane departed from the Deer Valley Airport, Phoenix, Arizona, for the cross-country personal flight. According to the pilot, he landed on runway 03. While taxiing to the terminal, the pilot did not see a 4-foot-deep ditch located in front of the terminal. The airplane impacted the ditch, and the right wing collided with the ground, resulting in damage to a stringer. The airport manager responded to the airport following the accident. The taxiway is designed with a centerline stripe and outer reflectors. The ditch is on a non-movement part of the airport approximately 45 feet from the edge of the taxiway. The taxiway is paved. From the taxiway there is a 1-inch drop, and rock chips cover the ground for an additional 15 feet, followed by dirt for the next 24 feet leading up to the ditch. The airport recently received a grant to reconstruct the taxiways, which will widen the taxiways and install taxiway lighting. The airplane collided with a ditch during taxi and sustained substantial damage. Night visual meteorological conditions prevailed. While taxiing to the terminal, the pilot taxied into a non-movement area of the airport, and did not see a 4-foot-deep ditch located in front of the terminal. The airplane impacted the ditch and the right wing collided with the ground, resulting in damage to a stringer. The ditch was approximately 45 feet from the taxiway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_LAX05CA001.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). 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 …
- 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…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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