NTSB CAROL · Event
Event CHI02LA118
Registry · N6RP
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-6
Year of manufacture
2006
Engine
SUBARU ALL MDLS A/B (400 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20060825
ADS-B equipped
Yes — Mode-S A7C412
Registrant of record
LANDRUM KELLY T
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The inadequate weather evaluation and delayed application of carburetor heat by the pilot, and the unsuitable terrain encountered during the forced landing. The carburetor icing conditions and the low altitude were factors.
Factual narrative
On April 30, 2002, at 0810 central daylight time, a Cessna 120, N6RP, piloted by a private pilot, was substantailly damaged when it struck a building while approaching to land on runway 32 (4,423 feet by 100 feet, asphalt), at the John H. Batten Airport (RAC), Racine, Wisconsin. The pilot reported that, while in the traffic pattern, the engine lost power. The 14 CFR Part 91 personal flight was operated in visual meteorological conditions, and was not on a flight plan. The pilot, who was the sole occupant, received minor injuries. The local flight originated from the Sylvania Airport, Sturtevant, Wisconsin, at 0730. In his written statement, the pilot said he took off at 0730 to, "...continue my break-in of my newly overhauled engine. This flight was the 7th hour since [major overhaul]." The pilot said that he decided to fly the airplane to RAC. He said that when he was 6.5 to 7 miles southwest of RAC he switched to the right fuel tank. He said the right fuel tank was "fullest". The pilot said that the the engine stopped developing power in the traffic pattern as he approached a position 45 degrees from his intended touchdown point. He said the power loss happened as he was making a power reduction. The pilot said that he verified the carburetor heat and magneto switch positions and he then attempted to restart the engine. The pilot stated that he had applied carburetor heat at, "...midpoint on downwind." The pilot said that he was in an area with, "...too many homes between [his] location and the [airport]." The airplane struck a building during the forced landing. A postaccident examination of the airplane was conducted by a Federal Aviation Administration inspector. Fuel was found in both wing fuel tanks. The fuel selector and fuel lines were examined and no blockage or other pre-impact anomalies were found. No fuel contamination was found. Engine valve train continuity was established by rotating the engine crankshaft. "Thumb" compression was exhibited on all cylinders. Spark was observed for the top spark plug leads during engine rotation. The magneto switch was checked with a multi-meter and no disrepencies were found. The carburetor was broken loose from the induction manifold. No other anomalies were found with respect to the carburetor. No anomalies were found with respect to the airframe, engine, or systems that could be identified as existing prior to impact. The weather at RAC at 0753 was: Winds - 290 degrees magnetic at 11 knots; Visibility - 10 statute miles; Sky condition - clear; Temperature - 9 degrees Celsius; Dew Point - 1 degree Celsius; Altimeter setting - 29.91 inches of Mercury. According to a carburetor icing probability chart, the temperature and dew point were in the range of serious icing at descent power or moderate icing at cruise power. The Federal Aviation Administration and Teledyne Continental Motors were parties to the investigation. The airplane struck a building during a forced landing following a loss of engine power during a landing approach. The pilot said that when he was 6.5 - 7 miles from his destination, he switched to the right fuel tank. He said the right fuel tank was "fullest". He reported that the engine stopped developing power as he neared the base leg of the traffic pattern. He said the power loss happened as he was making a power reduction. The pilot said that he verified the carburetor heat and magneto switch positions and he then attempted to restart the engine. The pilot stated that he had applied carburetor heat at, "...midpoint on downwind." The pilot said that he was in an area with, "...too many homes between [his] loaction and the [airport]." No anomalies were found with respect to the airframe, engine, or systems that could be identified as existing prior to impact. The weather at the destination airport listed a temperature of 9 degrees Celsius and a dew point of 1 degrees Celsius. According to a carburetor icing probability chart, the temperature and dew point were in the range of serious icing at descent power or moderate icing at cruise power. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI02LA118.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 (icing, fuel contamination). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2024 · arXiv preprint
Mechanisms of de-icing by surface Rayleigh and plate Lamb acoustic waves
Acoustic waves (AW) have recently emerged as an energy-efficient ice removal procedure compatible with functional and industrial-relevant substrates.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
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