ATL03LA121
2003-07-30 · Fort Payne, Alabama, United States · Minor · 1 aircraft · Status: Completed
Airport 4A9
Aircraft involved
Probable cause & findings
The pilot's failure to properly reconnect the mixture control cable resulting in a total loss of engine power, and subsequent in-flight collision with the trees.
Factual narrative
On July 30, 2003, at 1100 central daylight time, a Lancair 235, N7156W, registered to and operated by a commercial pilot, collided with the ground following a complete loss of engine power at Isbell Field, Ft. Payne, Alabama. The personal flight was conducted under the provisions of Title 14 CFR Part 91.Visual meteorological conditions prevailed at the time of the accident. The airplane was substantially damaged and the pilot received minor injuries. The flight departed Isbell Field, Ft. Payne, Alabama, on July 30, 2003, at 1030. According to the pilot, he removed the carburetor from the accident airplane to trouble-shoot another airplane. He reinstalled the carburetor on the accident airplane, and flew it for approximately 20 minutes. While on final approach to land on runway 4, the engine quit. The airplane collided with trees during an attempted emergency landing. Examination of the engine revealed no mechanical malfunctions. Examination of the carburetor control system revealed that the mixture control cable was not connected. The mixture control arm on the carburetor was in the idle cut-off position. According to the pilot, he removed the carburetor from the accident airplane to troubleshoot another airplane. He reinstalled the carburetor on the accident airplane, and flew it for approximately 20 minutes. While on final approach to land on runway 4, the engine lost power. The airplane collided with trees during an attempted emergency landing. Examination of the engine revealed no mechanical malfunctions. Examination of the carburetor control system revealed that the mixture control cable was not connected. The mixture control arm on the carburetor was in the idle cut-off position. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_ATL03LA121.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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…