NTSB CAROL · Event
Event ERA12CA348
Aircraft involved
Probable cause & findings
The pilot's improper fuel management, which resulted in a total loss of engine power during approach due to fuel exhaustion.
Factual narrative
The pilot reported that the airplane had been flying about 4 hours, 25 minutes since its last fueling, which included two takeoffs and climbs. Toward the end of a long cross-country flight, during approach to the destination airport, the engine lost all power. At that time, the airplane was approximately 3 miles from the destination airport at 1,200 feet above ground level. The fuel selector was positioned to the left main fuel tank when the power loss occurred. The pilot moved it to the right main fuel tank, but the engine did not regain power. The pilot then performed a forced landing to a road. During the landing, he had to veer left to avoid an automobile and the left wing impacted a median. The airplane spun 180 degrees and came to rest upright. Examination of the wreckage by a Federal Aviation Administration inspector revealed substantial damage to both wings. The inspector noted that the left wing fuel tank was intact and did not contain any fuel. The right wing fuel tank had been compromised; however, it was only compromised on the top of the tank and no fuel leaked from the right main fuel tank. The inspector observed approximately 1/2 gallon of fuel in the right main fuel tank. The inspector did not observe and mechanical malfunctions that would have contributed to the loss of engine power, nor did the pilot report any. The pilot reported that the airplane had flown about 4 hours, 25 minutes, including two takeoffs and climbs, since its last fueling. When the airplane was about 3 miles from the destination airport at 1,200 feet above ground level, the engine lost all power. The fuel selector was positioned to the left main fuel tank when the power loss occurred. The pilot moved the selector to the right main fuel tank, but the engine did not regain power. The pilot then performed a forced landing to a road. During the landing, he veered left to avoid an automobile and the left wing impacted a median. The airplane spun 180 degrees and came to rest upright. Postaccident examination of the wreckage revealed no evidence of mechanical malfunctions or failure that would have precluded normal operation; however, there was impact-related damage to both wings. The left main fuel tank was intact and did not contain any fuel. Although the top of the right main fuel tank had been compromised, there was no evidence that fuel had leaked from that tank. About 1/2 gallon of fuel was found in the right main fuel tank. 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 management - C
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA12CA348.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). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- AOPA Air Safety Institute 2023 · Safety advisor
Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- NASA NTRS 2019 · Abstract
U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR)
A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other
Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …
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