NTSB CAROL · Event
Event CHI94LA084
Aircraft involved
Probable cause & findings
THE PILOT'S POORLY PLANNED APPROACH AND REMAINING BELOW A PROPER GLIDE PATH DURING FINAL APPROACH. THE PILOT'S LACK OF TOTAL EXPEREINCE WAS A FACTOR.
Factual narrative
On February 13, 1994, at 1633 hours central standard time, a Piper Tomahawk PA-38-112, N23797, operated as a rental aircraft by Thunderbird Aviation, Inc., of Minneapolis, Minnesota, impacted static lines between power poles on final approach to Runway 27R at Flying Cloud Airport, Eden Prairie, Minnesota. A section of the right wing leading edge and upper surface departed the aircraft. The aircraft came to rest approximately 300 feet further on the flight path and was destroyed. The pilot was seriously injured. Visual meteorological conditions prevailed at the time of the accident and a VFR flight plan was on file. The flight was operated under 14 CFR Part 91, and originated from Eden Prairie, MN, as a student solo cross country. At 1550 hours the pilot departed on a return leg from a refueling stop at Olivia, MN (Y39). A review of the Air Traffic Control tape indicates the pilot initially contacted the tower and incorrectly reported his position as 10 miles southwest of tha airport. Initial tower instructions were to expect a landing on runway 27L. The tower determined the airplanes' actual position to be north-northwest of the airport using tower radar. The controller gave the pilot vectors to the field and handed him off to the north tower controller. The pilot was cleared to land on runway 27R. An aircraft in the pattern following the mishap aircraft asked the tower what the Tomahawk's intentions were. The tower controller responded that he was landing. The tower controller then asked the Tomahawk if he still had the airport in sight, to which the pilot responded, "Roger, making final." The tower controller cautioned "you're a little bit low, you might want to pull up." The following traffic then notified the tower that he saw the mishap aircraft hit the wires. There were no visual markers on the wires. The supporting towers were marked with red obstruction lights. The approximate height of the wires were 950 ft above mean sea level(MSL). The runway threshold elevation is 906 ft MSL. The distance from the threshold was approximately 7250 ft. No VASI was installed on Runway 27R. Sunset was at 1738 central standard time. The airplane had accrued 8 hours since annual inspection, where no discrepancies were noted. Post crash inspection of the aircraft showed presence of fuel at the site, engine continuity, flight control continuity and the ability of the undamaged magneto to produce spark. The FAA Airworthiness Inspector's on scene report is enclosed. WHILE ON FINAL APPROACH TO THE ORIGINATING AIRPORT AFTER A SOLO CROSS COUNTRY FLIGHT, THE AIRPLANE STRUCK UNMARKED POWERLINES. THE AIRPLANE THEN DESCENDED TO IMPACT WITH THE TERRAIN. THE POWERLINES WERE LOCATED 1.2 MILES FROM THE RUNWAY THRESHOLD AND WERE 44 FEET ABOVE THE RUNWAY ELEVATION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_CHI94LA084.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). 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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