NTSB CAROL · Event
Event WPR24LA063
Registry · N111XF
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-6
Year of manufacture
1997 · 27 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19971009
ADS-B equipped
Yes — Mode-S A031FD
Registrant of record
BENDER THOMAS G
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A loss of engine power for undetermined reasons.
Factual narrative
On January 2, 2024, at 1030 mountain standard time, an experimental amateur-built Vans RV-6, N111XF, was substantially damaged when it was involved in an accident near Moriarty, New Mexico. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that the airplane operated normally through preflight and initial takeoff. Shortly after becoming airborne, and while still over the runway, the engine began to “stutter” and lose power. The pilot turned on the electric fuel pump, but the engine did not respond. During the forced landing that followed, the airplane exited the runway and the landing gear collapsed, substantially damaging the fuselage. The pilot reported that 6 to 12 months before the accident, he had experienced a similar instance of an engine failure during takeoff, but he was able to land during that instance. He determined that the fuel pump had failed and he replaced the failed fuel pump at that time with one that he reported had been originally installed on a Lycoming engine when he rebuilt it in 1954. Attempts to contact the pilot to access the airplane and engine for an examination were unsuccessful. The airframe and engine logbooks were not located during the investigation. According to FAA inspectors, the pilot had not completed a biannual flight review “in decades” and his last recorded application for a medical certificate was denied in 2009. The pilot reported that the airplane was operating normally throughout the preflight and initial takeoff. Shortly after becoming airborne, and while still over the runway, the engine began to “stutter” and lose power. The pilot turned on the electric fuel pump, but the engine did not respond. During the forced landing that followed, the airplane exited the runway and the landing gear collapsed, substantially damaging the fuselage. The pilot stated that 6 to 12 months before the accident he had experienced a similar instance of an engine failure during takeoff, but he was able to land during that instance. He attributed that loss of power to a failed fuel pump. He stated that he replaced the failed fuel pump with a used fuel pump that was on an engine that he rebuilt 70 yrs ago. Attempts to contact the pilot to access the airplane and engine for an examination were unsuccessful. Although the fuel pump was reportedly 70 yrs old, investigators could not determine if it failed. Therefore, the reason for the loss of engine power could not be determined. 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).
- — Aircraft-Aircraft power plant-(general)-(general)-Unknown/Not determined
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Attain/maintain not possible
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR24LA063.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, engine failure). 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
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- 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…
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