NTSB CAROL · Event
Event CHI05LA015
Registry · N230SB
FAA Aircraft Registry record.
Make / Model
LYDDON S/LYDDON W LYDDON PITTS S1S
Year of manufacture
2011
Engine
LYCOMING O-360 SERIES (180 hp)
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20110924
ADS-B equipped
Yes — Mode-S A20A12
Registrant of record
SIERRA BRAVO PARTNERSHIP
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain control of the airplane while performing aerobatic flight maneuvers resulting in an in-flight collision with terrain.
Factual narrative
On October 24, 2004, about 1430 central daylight time, an experimental amateur-built Strissel Pitts S1S bi-wing airplane, N230SB, was substantially damaged during an in-flight collision with terrain near Liberal, Kansas. The personal flight was being conducted under 14 CFR Part 91 and was not on a flight plan. Visual meteorological conditions prevailed. The pilot sustained fatal injuries. The local flight departed Liberal Municipal Airport (LBL), Liberal, Kansas, about 1400. A witness reported seeing a small airplane go into a "backward spin, then it flipped up side down and stayed [in] a spin until it disappeared over the hill." A second witness stated that he saw an airplane "doing tricks." He continued: "I watched him for a few minutes, then he was doing this crazy stunt up in the air. He was upside down going in circles. And I was noticing that he was getting closer to the ground. Then all of a sudden he wasn't pulling up." He noted the airplane descended until it impacted the ground. The airplane came to rest inverted on level terrain approximately 2 miles west-southwest of LBL. The engine cowling, upper wing assembly, and vertical stabilizer exhibited crushing damage. The flight controls remained attached to the airframe. Control continuity was confirmed from the empennage to the cockpit area and from the ailerons to the wing roots. Cable breaks exhibited a frayed condition consistent with overload tensile failure. One of the co-owners of the aircraft reported that they had owned it for approximately 20 years. They were reportedly in the process of negotiating a trade with the accident pilot involving the aircraft. During this time, the owner stated that the accident pilot had permission to fly the Pitts aircraft. He noted that the accident pilot had told him that he had experience in two-seat Pitts aircraft and with aerobatics in general. The owner stated that he had flown the accident aircraft the evening prior to and the morning of the accident. He reported that he conducted some takeoffs and landings during the evening flight and performed some aerobatic work during the morning flight. He stated that the aircraft performed normally. He noted that he was not aware of any discrepancies with the aircraft. Federal Aviation Administration records indicate the accident pilot held a private pilot certificate with a single-engine land rating. He also held a mechanic certificate with airframe and powerplant ratings. He was issued a third class airman medical certificate on November 11, 2002. His pilot logbook was not located. He reported his total flight time as 1,000 hours on his medical certificate application. The experimental amateur-built airplane was substantially damaged and the pilot fatally injured during an in-flight collision with terrain. Witnesses reported that the aircraft was conducting aerobatic airwork when it entered an inverted spin. According to one witness, the airplane went into a "backward spin, then it flipped up side down and stayed [in] a spin until it disappeared over the hill." A second witness stated the airplane was "doing tricks." He reported the airplane was "upside down going in circles" and did not recover prior to impact. The airplane came to rest inverted. The flight controls remained attached to the airframe. Control continuity was confirmed from the empennage to the cockpit area and from the ailerons to the wing roots. Cable breaks exhibited a frayed condition consistent with overload tensile failure. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_CHI05LA015.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). 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 · 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…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗