NTSB CAROL · Event
Event ERA11CA069
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight/inflight fuel planning resulting in fuel exhaustion and total loss of engine power.
Factual narrative
According to the pilot, he reviewed the weather prior to departing on the 416-nautical mile cross-country flight. The pilot fueled the airplane with 30.1 gallons of fuel the morning of the flight. About 3 miles from the destination airport, descending through 1,500 feet msl, the engine sputtered and then lost power. During a forced landing on a grassy area, the airplane struck a tree, continued down an incline, and came to rest in a small pond, sustaining substantial damage to the fuselage, both wings, and the firewall. Examination by a Federal Aviation Administration inspector revealed that the airplane's left fuel tank contained 2.5 gallons of fuel, the right fuel tank contained 0.5 gallons of fuel, and the fuel selector was in the "BOTH" position. Review of the Cessna Model 172 Owner's Manual revealed that, the maximum usable fuel capacity in all flight conditions was 36 gallons; however, unusable fuel in level flight was 0.5 gallons. At 67 percent power, and operating with a lean mixture, the airplane's fuel consumption rate was 7.6 gallons per hour but, according to the manual, Allowances for fuel reserve, headwinds, take-offs, and climb, and variations in mixture leaning technique should be made and are in addition to those shown on the charts. Other indeterminate variables such as carburetor metering-characteristics, engine and propeller conditions, and turbulence or atmosphere may account for variations of 10 percent or more in maximum range. When asked how the accident could have been prevented, the pilot stated that he should have stopped for fuel en route. According to the pilot, he reviewed the weather prior to departing on the 416-nautical mile cross-country flight. The pilot fueled the airplane with 30.1 gallons of fuel the morning of the flight. About 3 miles from the destination airport, as the airplane was descending through 1,500 feet mean sea level, the engine sputtered and subsequently experienced a loss of power. During the forced landing, the airplane struck a tree, continued down an incline, and came to rest in a small pond, sustaining substantial damage to the fuselage, both wings, and the firewall. A postaccident examination by a Federal Aviation Administration inspector revealed that the airplane's left fuel tank contained 2.5 gallons of fuel, the right fuel tank contained 0.5 gallons of fuel; the fuel selector was in the "BOTH" position. A review of the airplane's applicable Owner's Manual revealed that the unusable fuel in level flight was 0.5 gallons. At 67 percent power, and operating with a lean mixture, the airplane's fuel consumption rate was 7.6 gallons per hour. When asked how the accident could have been prevented, the pilot stated that he should have stopped for fuel en route. 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 Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C
- C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid level - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA11CA069.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 (fuel exhaustion, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2026 · arXiv preprint
Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
- arXiv 2025 · arXiv preprint
Explainable LiDAR 3D Point Cloud Segmentation and Clustering for Detecting Airplane-Generated Wind Turbulence
Wake vortices - strong, coherent air turbulences created by aircraft - pose a significant risk to aviation safety and therefore require accurate and reliable detection methods.
- arXiv 2024 · arXiv preprint
Does small-scale turbulence matter for ice growth in mixed-phase clouds?
Representing the glaciation of mixed-phase clouds in terms of the Wegener-Bergeron-Findeisen process is a challenge for many weather and climate models, which tend to overestimate this process because…
- arXiv 2023 · arXiv preprint
Effects of electrostatic interaction on clustering and collision of bidispersed inertial particles in homogeneous and isotropic turbulence
In sandstorms and thunderclouds, turbulence-induced collisions between solid particles and ice crystals lead to inevitable triboelectrification.
- SKYbrary (Eurocontrol) 2023 · SKYbrary article
Wake Vortex Turbulence — SKYbrary Knowledge Base
SKYbrary wake vortex turbulence comprehensive article — generation mechanics, dissipation factors, separation standards (ICAO LIGHT/MEDIUM/HEAVY/SUPER + recategorisation RECAT-EU).
Browse the full corpus — academia portal ↗