NTSB CAROL · Event
Event CEN23LA226
Registry · N3830K
FAA Aircraft Registry record.
Make / Model
TEMCO GC-1B
Year of manufacture
1948 · 75 years old at event
Engine
CONT MOTOR 0-300 SER (145 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19550908
ADS-B equipped
Yes — Mode-S A468D1
Registrant of record
BRIAN ENGINEERING & CONSULTING PLLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power due to carburetor ice due to the pilot’s delayed application of carburetor heat.
Factual narrative
On June 3, 2023, about 1635 central daylight time, a Temco GC-1B airplane, N3830K, was substantially damaged when it was involved in an accident near Bristow, Oklahoma. The pilot sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot stated that he was enroute to a friend’s private grass strip airport (OK69) to practice touch-and-go landings. A witness observed the airplane approach OK69 from the north about 300 ft above ground level. The airplane was in a shallow left turn, and the engine was running rough. He said that the engine lost and regained rpms about four times before it stopped running. The airplane appeared to be flying slowly. The witness lost visual contact with the airplane behind some trees. Seconds later, he heard the airplane make sudden and audible contact with the ground and he immediately called the police department and went to the accident site. According to the witness, the pilot was sitting up and unbuckled in the left seat and was unclear as to where he was or how he got there. The pilot asked questions as to what had occurred; he kept telling the witness that all he could remember was that the engine was running rough and that he was trying to correct the problem. He thought that the engine had carburetor ice, so he applied carburetor heat, but the engine roughness got worse The airplane wreckage was found lying level in a vegetated area. The front portion of the cockpit and the wings were crushed aft. The examination of the airframe, flight controls, fuel system, and engine did not reveal any pre-impact anomalies that would have precluded normal operations. The Federal Aviation Administration’s Special Airworthiness Information Bulletin CE-09-35 includes a carburetor icing probability chart. Using the nearest reported temperature of 26° C, and a dew point of 17° C, the chart indicated that the airplane was operating in weather conditions conducive to serious carburetor icing at glide power. The pilot was enroute to a private grass airstrip to practice touch-and-go landings. A witness observed the airplane approach the airstrip about 300 ft. The airplane was in a shallow left turn and the engine was running rough. He said that the engine lost and regained rpms about four times before it stopped running. The airplane appeared to be flying slowly. Seconds later, the witness heard the airplane make a sudden and audible contact with the ground, and he went immediately to the accident site. The airplane was lying upright in a vegetated field with the forward part of the fuselage and wings substantially damaged. The pilot told the witness that all he could remember was that the engine was running rough and that he was trying to correct the problem. The pilot said that he thought that he had carburetor ice, so he applied carburetor heat, but the engine roughness got worse. Examination of the airframe, flight controls, fuel system, and the engine, did not reveal any pre-impact anomalies that would have precluded normal operations. The airplane was being operated in weather conditions conducive to serious carburetor icing at glide power. Based on the pilot’s and the witness’s recollection of the event and the weather conditions, the loss of engine power was most likely the result of carburetor icing due to the pilot’s delayed application of carburetor heat. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-Conducive to carburetor icing-Contributed to outcome
- — Aircraft-Aircraft power plant-Engine (reciprocating)-(general)-Malfunction
- — Personnel issues-Action/decision-Action-Delayed action-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2023_CEN23LA226.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 ↗