NTSB CAROL · Event
Event CHI02LA278
Registry · N54LF
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-8A
Year of manufacture
2002 · 0 years old at event
Engine
LYCOMING O-360 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20020511
ADS-B equipped
Yes — Mode-S A6D693
Registrant of record
FRANK LORIN L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The failure of the nose landing gear strut for undetermined reasons.
Factual narrative
On September 10, 2002, at 1230 central daylight time, an amateur-built Frank RV-8A, N54LF, sustained substantial damage during landing at the Brodhead Airport, Brodhead, Wisconsin. During the landing, the nose landing gear strut bent rearward and the airplane nosed over. The 14 CFR Part 91 personal flight was conducted in visual meteorological conditions without a flight plan. The private pilot was not injured and his passenger received minor injuries. The flight originated from the Rock County Airport, Janesville, Wisconsin at 1210. The pilot stated in a written report that the landing touchdown was normal and on the mains with the nose held off of the ground until the airplane slowed down. He said that the nose landing gear touched a small bump and then collapsed. The airplane subsequently nosed over. Examination of the airplane revealed that the nose landing gear strut had bent smoothly through about 90 degrees. The nose landing gear of the airplane is installed in a tube mount and angles forward and downward from the firewall area. The forward end of the strut is machined to accept a castoring nose wheel assembly. No defects were found in the caster assembly, or in the upper mount near the firewall. During landing on a turf runway, the nose landing gear strut bent rearward and the airplane nosed over. The pilot stated that the landing touchdown was normal and on the mains with the nose held off of the ground until the airplane slowed down. He said that the nose landing gear touched a small bump and then collapsed. The airplane subsequently nosed over. Examination of the airplane revealed that the nose landing gear strut had bent smoothly through about 90 degrees. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI02LA278.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 ↗