NTSB CAROL · Event
Event ERA18LA239
Registry · N628X
FAA Aircraft Registry record.
Make / Model
CHARLES JOSEPH ROSS MK-4
Year of manufacture
2016 · 2 years old at event
Engine
ROTAX 912UL (80 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20190404
ADS-B equipped
Yes — Mode-S A83602
Registrant of record
BOWEN AUSTIN
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power for reasons that could not be determined based on the available information.
Factual narrative
On August 30, 2018, about 1530 eastern daylight time, an experimental, amateur-built Avid MK-4, N628X, was substantially damaged when it was involved in an accident near Harnett, North Carolina. The private pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The airplane was equipped with a 10-gallon fuel tank in each wing; however, the left wing tank had been previously capped due to a fuel contamination issue and was not in use during the accident flight. The pilot noted during his preflight inspection that there were about 9 gallons of automotive gas in the right tank, which he said, "should have been sufficient" for the 35-nautical-mile flight. The pilot stated that, less than 30 minutes into the flight, he noted that the fuel level had decreased below about half, which he described as abnormal, and he diverted to Harnett Regional Jetport Airport (HRJ), Harnett, North Carolina to refuel; however, during the descent, the engine lost total power. He turned on the auxiliary fuel pump but was unable to restart the engine, and subsequently performed a forced landing in a field. After touchdown, the airplane nosed over and came to rest inverted, resulting in substantial damage to the wings and fuselage. The pilot turned the fuel selector to the OFF position after the accident. According to the Federal Aviation Administration (FAA) inspector who performed an examination of the airplane, fuel was present on the ground under the right wing tank. When the airplane was recovered, fuel poured out of the wings, and about 1/2 gallon of fuel was captured from the right tank. The electric fuel pump was turned on and operated normally. All fuel lines were intact and a small amount of debris was noted. The engine's crankshaft was rotated by hand, and internal and valvetrain continuity was established. Examination of the airplane and engine revealed no evidence of preimpact mechanical anomalies that would have prevented normal engine operation. On the Pilot/Operator Aircraft Accident/Incident Report (NTSB form 6120.1/2), the pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Furthermore, in the "Operator/Owner Safety Recommendation" section of the report, he stated, "ensure that Avid and Kitfox aircraft wing tank fuel caps are vented with a forward facing 1 1/2 tube as per Kitfox Service Letter #7,” which was issued on May 6, 1997. The accident airplane's right wing fuel tank was vented by a modified fuel cap; holes were drilled in the top of the cap to allow air in the tank as fuel was consumed. The pilot departed on a 35-nautical-mile flight with 9 gallons of fuel onboard. While en route, he noticed that the fuel quantity was decreasing faster than normal, and he elected to stop for fuel. During the descent toward the airport, the engine lost total power and the pilot subsequently performed a forced landing in a field. After touchdown, the airplane nosed over and came to rest inverted, resulting in substantial damage to the wings and fuselage. Examination of the airplane and engine revealed no evidence of preimpact mechanical anomalies that would have prevented normal engine operation. About 1/2 gallon of fuel was drained from the fuel tank after the accident; however, an unquantified amount spilled onto the ground during recovery, and the amount of fuel onboard at the time of the accident could not be determined. The right wing fuel tank was vented by a modified fuel cap. Holes were drilled in the top of the cap to allow air in the tank as fuel is consumed. The pilot recommended that a forward-facing tube vent be installed per a service letter issue by the kit manufacturer of a similar experimental, amateur-built airplane; however, the reason for loss of engine power and whether the modified fuel cap contributed to the accident could not be determined based on the available information. 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 Not determined-Not determined-(general)-(general)-Unknown/Not determined
Verbatim from NTSB's published report. Source file
NTSB_2018_ERA18LA239.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, fuel contamination). 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…
Browse the full corpus — academia portal ↗