NTSB CAROL · Event
Event WPR15LA218
Registry · N810GL
FAA Aircraft Registry record.
Make / Model
TURBINE CUBS OF WYOMING PA-18
Year of manufacture
2009 · 6 years old at event
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20090204
ADS-B equipped
Yes — Mode-S AB09FD
Registrant of record
DAFOE GERALD W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A gouge in the right brake master cylinder piston O-ring, which resulted in a loss of brake pressure and reduced effectiveness after landing. Contributing to the accident was the pilot’s decision to operate the airplane with an ongoing brake issue.
Factual narrative
On July 14, 2015, at 1030 mountain daylight time, a Dafoe TCOW Smith Cub, N810GL, ground looped after landing, collapsing the right landing gear and substantially damaging the right wing. The private pilot was not injured. The airplane was registered to the pilot, and was operated as a personal flight under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the flight, and no flight plan had been filed. The pilot stated to the NTSB investigator that after landing he applied brakes to slow the airplane. He did not feel any right brake resistance, and the airplane swerved left due to left brake application. He attempted to correct with rudder but the airplane ground looped to the left, collapsing the right landing gear, and damaging the right wing. An FAA inspector examined the airplane and the brake system. He did not note any unusual wear on the pins or brake pads. He did note that the owner had installed an additional brake fluid reservoir to the right brake master cylinder. There was no indication of brake fluid leak. The pilot/owner did state to the inspector that he had been having on-going issues with the right brake. The NTSB investigator authorized the pilot to disassemble and examine the right brake system. The pilot reported back that he found a gouge in the master cylinder piston o-ring that would allow brake fluid to bypass the seal. The private pilot/owner of the ultralight airplane was conducting a personal flight. He stated that, after landing, he applied the brakes to slow the airplane. He did not feel any right brake resistance, and the airplane swerved left due to left brake application. He attempted to correct with rudder inputs, but the airplane ground looped to the left, which resulted in the right landing gear collapsing and damage to the right wing. The pilot stated that the he had recently been having ongoing difficulty with the airplane's right brake function. Examination and disassembly of the right brake master cylinder revealed that the master cylinder piston O-ring had a gouge in it. The gouge likely allowed brake fluid to bypass the seal, which resulted in a loss of brake pressure and, therefore, reduced effectiveness after landing. 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 systems-Landing gear system-Brake-Malfunction - C
- C Aircraft-Aircraft systems-Landing gear system-Brake-Damaged/degraded - C
- F Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2015_WPR15LA218.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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