NTSB CAROL · Event
Event CHI02LA155
Registry · N46899
FAA Aircraft Registry record.
Make / Model
AERONCA 0-58B
Year of manufacture
1942 · 60 years old at event
Engine
CONT MOTOR A&C65 SERIES (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19560927
ADS-B equipped
Yes — Mode-S A5BB08
Registrant of record
FURLONG KELLY L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain adequate airspeed which resulted in a stall. A factor was the low altitude.
Factual narrative
On June 8, 2002, at 1211 central daylight time, an Aeronca 0-58B, N46899, piloted by a private pilot, was destroyed during an approach for landing at a private airstrip near Alexandria, Indiana. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal flight was not operating on a flight plan. The pilot and passenger were seriously injured. The flight originated from the Huntington Municipal Airport (HHG), Huntington, Indiana, at 1100, en route to Alexandria Airport (I99), Alexandria, Indiana. In a written statement, the pilot reported that he departed HHG to attend a luncheon at I99. He stated that the accident occurred on landing approach but due to head trauma he received, he was unable to remember specifics or details pertaining to the accident. In a written statement, the passenger reported that they entered the downwind from runway 27 and saw another airplane on short final. They continued the downwind and noted that another aircraft on the runway appeared that it would need more time to taxi off the runway as there were no taxiways. They continued on the downwind and then made a left hand turn, midfield, to set up for an overhead approach to allow for more spacing between them and the other aircraft which was now on the ground. While initiating the left hand turn, the airplane suddenly got into an unusual attitude. The left wing dipped down and the nose was pointed toward the ground. The pilot reported in his written statement that there was no mechanical malfunction failure. The airplane was resting about 20-30 feet to the side of runway 27 with its nose facing north. Ground scaring consisted of the area underlying the airplane. The nose of the airplane exhibited a nose down crush angle with no lateral deformation the airplane's empennage. Examination of the wreckage by the Federal Aviation Administration revealed no mechanical anomalies. The airplane impacted terrain 20-30 feet from the side of the landing runway while the pilot was initiating a left hand turn during the downwind segment of the visual approach. The passenger stated that the airplane's left wing dropped and the nose pitched down during the turn. Ground scarring was limited to an area near the main wreckage, which exhibited a nose down crush angle with no lateral bending of the empennage. No mechanical anomalies were noted. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI02LA155.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 ↗