ERA11CA423
2011-07-26 · Quinton, Virginia, United States · Minor · 1 aircraft · Status: Completed
Airport RIC
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight planning and fuel management, which resulted in a total loss of engine power due to fuel exhaustion.
Factual narrative
Originally the pilot was going to depart earlier on the day of the accident and had planned to stop enroute to his destination for more fuel. After receiving a weather briefing he decided instead to delay his departure until later that evening due to the possibility of thunderstorms being present at his time of arrival in the vicinity of his destination airport. Prior to departure that evening he had the fuel tanks filled to capacity. During the flight despite his previous flight planning, he did not stop for more fuel. When he was approximately 64 miles from his destination, he noticed that his fuel gauges were indicating that he had less fuel than he anticipated. Upon arrival at his destination he flew an instrument approach and advised air traffic control that he was fuel critical, as he had exceeded his estimated flight time, his fuel gauges were indicating a low fuel state, and other aircraft were also landing. Due to the visibility, he was unable to see the runway environment and executed a missed approach. He was then instructed by Air Traffic Control to climb to 2,000 feet above mean sea level (msl). During the climb the engine lost power and the airplane began to descend. The pilot executed the engine restart procedure and was able to get the engine to restart. He then began climbing back up to 2,000 feet msl however, the engine lost power again. The airplane once again began to descend but this time; the pilot was unable to get the engine to restart. The airplane then struck trees and came to rest after falling approximately 20 feet to the ground. Total duration of flight was approximately 4 hours and 43 minutes. Post-accident examination of the airplane by a Federal Aviation Administration inspector revealed that the firewall and left wing were substantially damaged and both fuel tanks were absent of fuel. There was no evidence of any preimpact mechanical failure or malfunction of the airplane or engine. Correlation of radar and weather data revealed that the pilot for the majority of the flight would have encountered headwinds. The airplane was also not equipped with wheel fairings which according to the manufacturer would have further reduced its range by up to 7 percent. When asked how the accident occurred by a state trooper, the pilot advised him that he had run out of fuel. Originally the pilot was going to depart earlier on the day of the accident and had planned to stop enroute to his destination for more fuel. After receiving a weather briefing, he decided to delay his departure until later that evening due to the possibility of thunderstorms being present in the vicinity of his destination airport at his planned time of arrival. Prior to departure that evening, he had the fuel tanks filled to capacity. During the flight, and despite his previous flight planning, he did not stop for more fuel. When he was approximately 64 miles from his destination, the pilot noticed that his fuel gauges were indicating that he had less fuel than he anticipated. Upon arrival at his destination, he flew an instrument approach and advised the air traffic controller that he was low on fuel. Due to the visibility, he was unable to see the runway environment and executed a missed approach. He was then instructed by the air traffic controller to climb to 2,000 feet mean sea level (msl). During the climb, the engine lost power and the airplane began to descend, but the pilot was able to restart the engine. He then began climbing back up to 2,000 feet msl; however, the engine lost power again. The airplane once again began to descend, but this time the pilot was unable to restart the engine. The airplane then struck trees and came to rest after falling approximately 20 feet to the ground. Total duration of the flight was approximately 4 hours and 43 minutes. Postaccident examination of the airplane revealed that the firewall and left wing were substantially damaged and both fuel tanks were absent of fuel. There was no evidence of any preimpact mechanical failure or malfunction of the airplane or engine. Correlation of radar and weather data revealed that the pilot would have encountered a headwind for the majority of the flight. When asked by a state trooper how the accident occurred, the pilot advised him that he had run out of fuel. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, 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_2011_ERA11CA423.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion, thunderstorm). All research papers
- Embry-Riddle Scholarly Commons 2024 · Journal article (IJAAA) The Impact of Thunderstorms on Take-off Data in South Africa
Aviation and meteorology are entwined disciplines, as aviation occurs in the atmosphere. Prevailing weather conditions at take-off are of utmost importance to aviation.
- NASA NTRS 2019 · Technical Memorandum (TM) Thunderstorm hazards flight research: Storm hazards 1980 overview
A highly instrumented NASA F-106B aircraft, modified for the storm hazards mission and protected against direct lightning strikes, was used in conjunction with various ground based radar and lightning…
- NASA NTRS 2019 · Conference Proceedings Operational evaluation of thunderstorm penetration test flights during project Storm Hazards '80
The National Aeronautics and Space Administration is conducting a research project called Storm Hazards '80 in order to study the prediction, detectability and avoidance of the hazards of severe storm…
- NASA NTRS 2019 · Preprint (Draft being sent to journal) Nowcasting Thunderstorm Anvil Clouds Over KSC/CCAFS
Electrified thunderstorm anvil clouds extend the threat of natural and triggered lightning to space launch and landing operations far beyond the immediate vicinity of thunderstorm cells.
- NASA NTRS 2019 · Contractor Report (CR) An Examination of Aviation Accidents Associated with Turbulence, Wind Shear and Thunderstorm
The focal point of the study reported here was the definition and examination of turbulence, wind shear and thunderstorm in relation to aviation accidents.
- NASA NTRS 2019 · Reprint (Version printed in journal) Observations of severe turbulence near thunderstorm tops
Data derived from the flight tapes of two airliners that experienced severe turbulence near thunderstorm tops are used to produce quantitative descriptions of the turbulence and its environment.