NTSB CAROL · Event
Event WPR24LA174
Registry · N1259M
FAA Aircraft Registry record.
Make / Model
BEECH 35-C33A
Year of manufacture
1967 · 57 years old at event
Engine
CONT MOTOR IO-520-B (285 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20200421
ADS-B equipped
Yes — Mode-S A069E4
Registrant of record
L A M CAPITAL MANAGEMENT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On June 1, 2024, at 1355 Pacific Daylight time, a Beech 35-C33A, N1259M, sustained substantial damage when it was involved in an accident near San Diego, California. The pilot and two passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. The pilot stated that the fuel tanks were full when he departed on the approximate 330 nm cross-country flight. He departed with the fuel selector positioned on the left tank and switched to the right fuel tank about 200 nm into the flight. As the airplane approached Montgomery-Gibbs Executive Airport, San Diego, an air traffic controller instructed the pilot to enter the left downwind leg of the traffic pattern for runway 28L and then to extend the leg 2 miles west of the airport. During the approach, he did not change the position of the fuel selector and noted that the fuel quantity gauges indicated that the right tank contained more fuel than the left. The auxiliary fuel pump was off as required by the checklist. The pilot further stated that on final approach, about one mile from the runway, he fully extended the flaps. Shortly thereafter, the engine experienced a partial loss of power and was “running rough.” The pilot attempted to troubleshoot the loss of power by enriching the mixture but was unable to restore engine rpm. The pilot determined he was too low to reach the runway and prepared to make a forced landing short of the runway. At about 20 ft above ground level (agl), the pilot flared and the stall warning horn sounded. The airplane touched down hard resulting in the nose gear collapsing. During the accident sequence, the left wing sustained substantial damage. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR24LA174.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 ↗