NTSB CAROL · Event
Event LAX02LA298
Aircraft involved
Probable cause & findings
A loss of engine power due to fuel exhaustion as a result of the pilot's inadequate fuel consumption calculations.
Factual narrative
On September 28, 2002, about 1000 Pacific daylight time, a Cessna 182, N6412A, experienced a loss of engine power in-flight, and collided with a tree during a forced landing near Lucerne Valley, California. The pilot was operating the airplane under the provisions of 14 CFR Part 91. The certified flight instructor and pilot-rated front-seated passenger received no injuries; the rear-seated passenger sustained minor injuries. The airplane sustained substantial damage. The personal cross-country flight departed the Boulder City Municipal Airport, Boulder City, Nevada, about 0845, with a planned destination of Apple Valley Airport, Apple Valley, California. Visual meteorological conditions prevailed, and a flight plan had not been filed. In a written statement, the pilot reported that prior to departure, he verified the airplane had 35 gallons of fuel onboard. While approaching Apple Valley, about 6,500 feet above ground level, the engine began to sputter. He verified that the fuel selector was in the "both" position, pulled the carburetor heat to the on position, and the engine smoothed out. About 10 to 15 seconds later, the engine began to surge, and then quit. He performed the engine failure in-flight emergency procedures, receiving help from the commercial pilot-passenger with completing checklist items. Unable to restart the engine, the pilot opted to land in a field, next to a busy highway. With full flaps, he approached the field about 65 to 70 miles per hour. Before touching down, he noticed a house directly in front of the airplane's path. He input left rudder and the airplane yawed to the left, away from the house and all other obstacles. The airplane touched down in a nose-high attitude, with the stall horn sounding. The airplane overran the field and continued across a dirt road. The left wing collided with a dead tree and the airplane impacted an embankment, collapsing the nose gear. After exiting the airplane, the pilot noted that there was a direct tailwind. He estimated the wind was about 25 to 30 knots, with gusts up to 40 knots. The Federal Aviation Administration inspector stated that he was unable to move forward with the investigation due to the airplane's owner leaving the country. He was also unable to locate the airplane's whereabouts, which prevented him from being able to conduct an examination of the airplane and engine. After the accident, an aircraft recovery service went to the accident site to remove the wreckage. During a telephone interview with the National Transportation Safety Board, the man recovering the wreckage stated that the airplane had come to rest in an upright position. Upon arrival, he noted that the fuel gauges, located by the wing in the upper cockpit area, both indicated empty tanks. The airplane's right wing was in good condition with the fuel tank intact. The airplane's left wing was damaged and the fuel tank's condition was undetermined. He found about 3 gallons of fuel in the left tank and about 4 gallons of fuel in the right tank. The airplane experienced a loss of engine power in-flight and collided with a tree during a forced landing. The pilot said that prior to departure he verified that the airplane had 35 gallons of fuel onboard. While approaching his planned destination, about 6,500 feet above ground level, the engine began to sputter. He verified that the fuel selector was in the "both" position, pulled the carburetor heat to the on position, and the engine smoothed out. About 10 to 15 second later, the engine began to surge, and then quit. Unable to restart the engine, the pilot opted to land in a field, next to a busy highway. After touching down, the airplane overran the field and continued across a dirt road. The left wing collided with a dead tree and the airplane impacted an embankment. After exiting the airplane, the pilot noted that there was a direct tailwind. He estimated the wind was about 25 to 30 knots, with gusts up to 40 knots. A representative of the company that recovered the wreckage after the accident stated that fuel tanks and lines were intact, and they drained about 3 gallons of fuel in the left tank and about 4 gallons of fuel in the right tank. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_LAX02LA298.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, 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.
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Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
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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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