N3830K is a 1948 Temco GC-1B. It is a fixed-wing single-engine aircraft with 2 seats, powered by a Cont Motor 0-300 SER rated at 145 horsepower. The registration is active, with the registrant based in Tulsa, OK. Its standard airworthiness certificate was issued in Sep 1955. It has been registered to its current owner since May 2023. This page also carries 1 NTSB event.
- 78 years old
- 1 of 119 Temco GC-1B
2023
1955
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N3830K's record changes.
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.
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