NTSB CAROL · Event
Event LAX99LA039
Aircraft involved
Probable cause & findings
Fuel exhaustion due to the pilot's failure to perform an adequate preflight of the aircraft to ensure that adequate fuel was available for the flight.
Factual narrative
On November 22, 1998, at 0928 hours mountain standard time, a Varga 2150A, N78114, lost power shortly before landing at the Chandler, Arizona, airport, and force landed in a residential area. During the landing, the aircraft collided with multiple ground obstructions. The aircraft, owned and operated by the pilot under 14 CFR Part 91, took off from Payson Arizona, about 0850 and was destined for Chandler. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft sustained substantial damage. Neither the private pilot nor the one passenger onboard was injured. In a written statement, the pilot stated that he was on a flight from Chandler to Payson with a planned return to Chandler. He reported there were no fuel services available in Payson and he departed for the return leg to Chandler. The pilot further stated he had an engine failure approximately 8 miles from the Chandler airport, over a residential farming area. The engine sputtered for several seconds and quit. The pilot attempted to restart the engine but was unsuccessful. He landed the airplane in a plowed field, crossed a road, collided with a street sign, and finally hit a residential block wall. In a phone interview on June 18, 1999, the pilot stated that he added 10 gallons of automotive fuel to top the tanks off before departing Chandler. The pilot further stated that there were no other mechanical malfunctions with the aircraft. The pilot said he did not perform a visual preflight check of the fuel quantity before departing Payson. The company that retrieved the aircraft, Air Transport of Phoenix, Arizona, documented the fuel system during disassembly of the aircraft for movement. All tanks, lines, and the fuel cap seals were intact. The fuel system was drained and a total of 4 ounces of fuel were found in the tanks and lines. The pilot had an engine failure while en route to his destination. He reported that there were no services available at the departure airport, and he did not perform a visual preflight check of the fuel tanks to determine quantity before departure. The engine failed approximately 8 miles from the airport, and the pilot made a forced landing in a residential farming area. The aircraft landed in a plowed field, proceeded to cross a road, hit a street sign, and finally hit a residential block wall. Upon examination, the fuel system continuity was established and a total of 4 ounces of fuel was found in the tanks and the lines. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_LAX99LA039.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, 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…
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