NTSB CAROL · Event
Event CHI02LA185
Aircraft involved
Probable cause & findings
The pilot's improper planning and decision making during the emergency descent and landing. The total loss of engine power due to fuel exhaustion and the pilot's inadvertent stall were contributing factors.
Factual narrative
On June 6, 2002, at 2051 central daylight time, an Eskildsen P, N2882, piloted by a private pilot, was substantially damaged during a forced landing following a total loss of engine power. The pilot was attempting to land on a street in Olathe, Kansas. 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 was uninjured. The local flight originated from the Johnson County Executive Airport (OJC), Olathe, Kansas, at 1940. The pilot stated in a written statement, "...Shortly after tower told me to report right base 18 the engine completely stop producing power, prop continues to windmill. The fuel gage( cork on a wire in fuel cap still showed more than a quarter tank of fuel in tank. I quickly pumped the throttle to active the carb pump and the engine responded with a couple of busts of power leading me to believe I was out of gas and only the fuel in the carb. bowl producing the temporary power. I had visual site of ojc and judged at me altitude of 3,500 [feet] I could not make the field." The pilot further stated, "...I approached 157thfrom the south 'midfield' on a heading of approx.340 degrees, with altitude and airspeed deteriorating rapidly , I was intensely concentrating on not stalling on my 'base to final' -270 degree heading, turn. Using nearly full input on both the rudder and ailerons to keep from rolling I made a somewhat skidding turn and missed lining up with the street by about 10 degrees. I came to a full stall I think about fifteen feet or so above the ground and pancaked onto a gravel parking lot springing the gear out both sides, slid about 15 feet over a 6 inch concrete curb wiping the gear completely into a retracted position. My upper and lower right wings struck a 6x6 wood porch post on the front of the building and started turning me in a clock wise direction. The second 6x6 post continued my rotation in a clock wise motion just as the prop and nosecone impacted the brick veneer front of the building. Upon striking the front of the building the aircraft bounced off of the building coming to rest about seven feet from the building with a heading of almost 180 from my approach. (sic)" The Federal Aviation Administration inspector's examination of the fuel system revealed that there was no fuel in the fuel tanks. The airplane was substantially damaged when it impacted a street and subsequently impacted a building during a forced landing following a total loss of engine power. The pilot stated in a written statement that he was at 3,500 feet agl when the engine quit and he determined that he could not make it to the airport. He stated that he missed lining up with the street he intended to land on by ten degrees. The pilot reported that he stalled the aircraft at 15 feet agl and that the landing gear buckled upon impact with the street. He stated that the airplane then slid into, and bounced off a building. The pilot stated that he believes that the fuel supply was exhausted. The Federal Aviation Administration inspector's examination of the fuel system revealed that there was no fuel in the fuel tanks. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI02LA185.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, fuel exhaustion). 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…
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