NTSB CAROL · Event
Event ERA15LA379
Aircraft involved
Probable cause & findings
The pilot's loss of airplane control, which resulted in a hard landing.
Factual narrative
On August 25, 2015, about 1335 eastern daylight time, an Engineering and Research Ercoupe 415-C, N87172, sustained substantial damage during a precautionary landing at the Newnan Coweta County Airport (CCO), Atlanta, Georgia. The airline transport rated pilot and the private pilot were not injured. The airplane was registered to and operated by the private pilot as a 14 Code of Federal Regulations Part 91 test flight. Visual flight rules conditions were reported at the time of the accident and no flight plan was filed for the local flight that departed from CCO about 1330. This was the airplane's first test-flight after having an annual inspection and its wings re-installed. The owner, who was a private pilot, said he performed the takeoff, but once it became airborne it banked hard left and the other pilot had to take control. The other pilot stated that he had to apply full right rudder and aileron to maintain level flight. He climbed to 400 ft with full power and turned back to land on the departure runway. Once the airplane was over the runway, the power was reduced and the airplane veered to the left. The pilot corrected for the yaw and the airplane yawed to the right and landed hard next to the runway. The nose gear collapsed and the airplane skidded to a stop damaging the propeller and an engine mount. A Federal Aviation Administration (FAA) inspector performed a postaccident examination of the airplane and found no mechanical deficiencies that would have precluded normal operation of the airplane's flight controls. The owner also reported that there were no mechanical problems and was unsure why the airplane was so hard to control. He suggested the wing attachments may have partially given-way but there was no way to prove this occurred. The 88-year old owner held a private pilot certificate for airplane single-engine land. He reported a total of 457 flight hours, of which, 270 hours were in the same make/model as the accident airplane. The owner's last FAA third-class medical was issued on December 3, 2012. The 52-year old pilot held an airline transport pilot rating for airplane multi-engine land, a commercial certificate for airplane single-engine land and instrument airplane, and a certified flight instructor rating for airplane single and multi-engine land. He was also a certified flight engineer with type ratings for BA-300 and DC-9 airplanes. The pilot reported a total of 7,500 flight hours, of which 50 were in the same make and model airplane as the accident airplane. His last FAA first-class medical was issued on March 10, 2015. Weather at the airport at 1355 was reported as wind 330 degrees at 4 knots, visibility 10 miles, and clear skies. The flight was being conducted by the private pilot/owner and an airline transport-rated pilot; it was the airplane's first test flight after an annual inspection and the reinstallation of the wings. The private pilot/owner reported that, after the airplane took off and became airborne, it banked hard left, and the other pilot took control. The other pilot stated that he had to apply full right rudder and aileron to maintain level flight. He climbed the airplane to 400 ft with full power and turned back to land on the departure runway. Once the airplane was over the runway, the pilot reduced the power, and the airplane again banked left. The pilot made a correction, and the airplane then banked right and landed hard next to the runway. A postaccident examination of the airplane revealed no mechanical deficiencies that would have precluded normal operation of the flight controls. The owner also reported that there were no mechanical problems with the airplane. He suggested that the wing attachments may have partially given-way, but no evidence was found indicating that this occurred. 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).
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2015_ERA15LA379.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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