NTSB CAROL · Event
Event LAX96LA024
Registry · N2167F
FAA Aircraft Registry record.
Make / Model
CESSNA U206
Year of manufacture
1965 · 30 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19650331
ADS-B equipped
Yes — Mode-S A1D31F
Registrant of record
SALE REPORTED
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the failure of the pilot to maintain control of the aircraft while maneuvering by visual reference to the surface in IFR conditions. An additional factor was the pilot's failure to continue with the missed approach.
Factual narrative
On October 27, 1995, at 0730 hours Pacific daylight time, a Cessna 206, N2167F, impacted the terrain adjacent to runway 7R while executing a circling approach in instrument meteorological conditions at Long Beach Airport, Long Beach, California. An instrument flight rules flight plan was filed. The aircraft was substantially damaged and the private pilot was uninjured. The business flight departed from Carlsbad, California, at 0630. The pilot told an NTSB investigator that, as he was en route, a fogbank was approaching the destination airport from the harbor area to the south. By the time he was established on the ILS Runway 30 approach about 5 miles southeast of the airport, the fogbank had reached the airport and obscured the runway 30 touchdown zone which is at the southern extremity of the airport. The pilot completed the ILS approach to minimums, and unable to acquire visual reference with the surface, initiated a missed approach. During the missed approach the pilot advised the tower that he had runway 7R in sight and the tower controller cleared the flight to land on that runway. While maneuvering in visual conditions, the pilot lost control of the aircraft, stalled at low altitude, and impacted terrain in a grass area approximately 1000 feet beyond the runway 7R threshold and 100 feet north of the runway centerline. THE AIRCRAFT IMPACTED TERRAIN ADJACENT TO THE DESTINATION RUNWAY WHILE EXECUTING A CIRCLING APPROACH IN INSTRUMENT METEOROLOGICAL CONDITIONS. THE PILOT COMPLETED AN INSTRUMENT LANDING SYSTEM APPROACH TO MINIMUMS AND EXECUTED A MISSED APPROACH. DURING THE MISSED APPROACH THE PILOT IDENTIFIED ANOTHER RUNWAY AND WAS CLEARED TO LAND ON THAT RUNWAY. WHILE MANEUVERING IN VISUAL CONDITIONS, THE PILOT STALLED THE AIRCRAFT AT A LOW ALTITUDE AND IMPACTED THE TERRAIN. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX96LA024.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…
Browse the full corpus — academia portal ↗