NTSB CAROL · Event
Event ERA24LA359
Registry · N9580S
FAA Aircraft Registry record.
Make / Model
CHAMPION 7ECA
Year of manufacture
1965 · 59 years old at event
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19650903
ADS-B equipped
Yes — Mode-S AD54C8
Registrant of record
SKYVAULT HOLDINGS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to properly secure the left wing fuel cap, which resulted in a total loss of engine power due to fuel exhaustion.
Factual narrative
The pilot was transporting the airplane from during a multi-leg trip and was on the second to last day of the trip. Prior to departure, he purchased fuel from a self-service pump and topped off both wing fuel tanks and checked that each fuel cap was properly secured. He calculated he had enough fuel for the 3.5 hour flight, plus a 40 to 50 minutes reserve, and departed. About 3 hrs. and 16 minutes into the flight, the engine lost total power. The pilot attempted to reach a nearby airport but made a forced landing about a mile short of the runway in trees, which resulted in substantial damage to the airplane’s right wing and tail section. Postaccident examination of the airplane revealed the left wing fuel cap was missing, and fuel streaks were observed aft of the cap toward the trailing edge of the wing. The left wing fuel tank was intact and empty of fuel. The right wing fuel cap was secure, and the tank was absent of fuel. The pilot stated that he did not have any issues with the fuel cap properly securing prior to the accident flight. The left fuel cap was never located. Based on available information, it is likely that the cap was not properly installed, and that it separated from the airplane at some point during the flight. Fuel was subsequently siphoned from the tank(s), and as a result, the engine lost power sooner than the pilot calculated due to fuel exhaustion. 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).
- — Personnel issues-Task performance-Inspection-Preflight inspection-Pilot
- — Aircraft-Aircraft systems-Fuel system-Fuel storage-Incorrect use/operation
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA24LA359.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 exhaustion). 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 ↗