NTSB CAROL · Event
Event WPR19LA003
Aircraft involved
Probable cause & findings
A loss of engine power due to fuel starvation and the pilot's mismanagement of the available fuel.
Factual narrative
On October 8, 2018, at 1100 Pacific daylight time, a Piper PA-28-161, N2250S, was substantially damaged when it was involved in an accident near Grass Valley, California. The student pilot was not injured. The airplane was operated as an instructional flight under the provisions of Title 14 Code of Federal Regulations Part 91. According to the pilot, she had completed three previous solo flights and this flight was her first cross-country flight. She planned the intended route from Auburn Municipal Airport (AUN) with intermediate landings at Lincoln Regional Airport (LHM), Colusa County Airport (O08), Willows/Glenn County Airport (WLW), Haigh Field Airport (037), Red Bluff Municipal Airport (RBL), and back to AUN. The pilot reported that before she departed AUN she confirmed the left fuel tank was full, and the right fuel tank was "to the tabs" (approximately 17 gallons). The airplane was not refueled during the cross-country flight. The pilot stated she flew with the left fuel tank selected for most of the flight; once she departed RBL, she switched to the right fuel tank (near Orville, California). When the airplane was about 5 miles from the Grass Valley Airport (GOO), at an altitude of about 5,000 ft above ground level (agl), the engine started to sputter. The pilot attempted, unsuccessfully, to restart the engine and she contacted the air traffic control tower at GOO to report an engine failure. She was cleared to land at GOO; however, the airplane was at an altitude of 3,200 feet agl and continuing to lose altitude. When she realized the airplane would not make it to the airport, she performed a forced landing to an open field. During the landing, the nose landing gear collapsed, and the right wing was damaged. Interviews with recovery personnel revealed that 17 gallons of fuel were removed from the rightwing fuel tank and the left-wing fuel tank was empty. Examination of the airplane by a Federal Aviation Administration inspector revealed no preimpact mechanical anomalies. The accident flight was the student pilot’s first solo cross-country flight; the intended route of flight included stops at five airports along the route. Prior to departure, the pilot confirmed the left fuel tank was full, and the right fuel tank contained about 17 gallons. The airplane was not refueled during the cross-country flight. The pilot stated she flew with the left fuel tank selected until the final leg of the trip. She report that, after departure from the last airport, she switched to the right fuel tank. When the airplane was about 5 miles from Grass Valley Airport (GOO), at an altitude of about 5,000 ft above ground level (agl), the engine started to sputter. The pilot attempted, unsuccessfully, to restart the engine and she contacted the air traffic control tower at GOO to report an engine failure. She was cleared to land; however, the airplane was at an altitude of 3,200 feet agl and continuing to lose altitude. When she realized the airplane would not make it to the airport, she performed a forced landing to an open field. During the landing, the nose landing gear collapsed, and the right wing was damaged. After the accident, 17 gallons of fuel were removed from the right-wing fuel tank and the left-wing fuel tank was empty. Because the amount of fuel in the right fuel tank after the accident was the same as before takeoff and the pilot stated she flew most of the flight with the left fuel tank selected, it is likely that, despite her report of switching to the right fuel tank, the left tank remained selected, and its fuel supply was exhausted. Other than the absence of fuel, no anomalies were noted with the engine that would have precluded normal operation. 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-Fluids/misc hardware-Fluids-Fuel-Fluid management
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Student/instructed pilot
Verbatim from NTSB's published report. Source file
NTSB_2018_WPR19LA003.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 starvation, 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.
- 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…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
Browse the full corpus — academia portal ↗