NTSB CAROL · Event
Event CEN17LA224
Aircraft involved
Probable cause & findings
The pilot’s difficulty controlling the airplane due to his incorrect reinstallation of the wings, which led to a bounced precautionary landing. Contributing to the accident was the failure of the pilot and the mechanic to verify the wings’ angle of incidence.
Factual narrative
On June 7, 2017, about 0930 central daylight time, an experimental amateur-built SD-1A airplane, N31313, was substantially damaged during a precautionary landing at Dodge County Airport (KUNU), Juneau, Wisconsin. The private-rated pilot was not injured. The personal flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no Federal Aviation Administration (FAA) flight plan had been filed for the flight. The local flight had departed about 0900. According to the pilot, immediately after takeoff the left wing felt "extremely heavy" and required an "exceptional amount of right aileron" to maintain level flight. The pilot was able to fly the airplane around the traffic pattern and perform a precautionary landing on runway 20. During the landing, the airplane bounced, and turned to the right. The left main landing gear collapsed, and the engine mount was substantially damaged. According to the FAA inspector who responded to the accident, the wings had been taken off the airplane prior to its purchase. The pilot purchased the airplane in April of 2016. During the reinstallation of the wings, in April of 2017, the pilot installed the wing bolts where he thought they should go. He did not perform any measurements during this reinstallation. The Airframe and Powerplant Mechanic who signed off on the condition inspection did not confirm the position of the wings and more specifically, the angle of incidence. The accident flight was the first flight after the reinstallation of the wings. Postaccident examination of the airplane revealed that the flight controls were continuous and correct; however, the angle of incidence, on the wings, was incorrect. No other anomalies were noted that would have precluded normal operation. The private pilot stated that, immediately after takeoff, the left wing felt "extremely heavy" and required "an exceptional amount of right aileron" to maintain level flight. During the precautionary landing, the airplane bounced, turned left, and the left main landing gear collapsed. The pilot had recently reinstalled the wings; however, he made no measurements during the reinstallation, and the mechanic who signed off on the condition inspection did not confirm the wings' angle of incidence. Postaccident examination of the airplane revealed that the angle of incidence was incorrect. Given this was the first flight since the reinstallation of the wings, it is likely the incorrect angle of incidence led to the pilot's difficulty controlling the airplane. 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 Aircraft-Aircraft structures-Wing structure-Flight surfaces (wing)-Incorrect service/maintenance - C
- C Personnel issues-Task performance-Maintenance-Installation-Pilot - C
- C Aircraft-Aircraft handling/service-Maintenance/inspections-(general)-Incorrect service/maintenance - C
- F Personnel issues-Task performance-Inspection-Post maintenance inspection-Pilot - F
- F Personnel issues-Task performance-Inspection-Post maintenance inspection-Maintenance personnel - F
Verbatim from NTSB's published report. Source file
NTSB_2017_CEN17LA224.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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