NTSB CAROL · Event
Event IAD04CA002
Aircraft involved
Probable cause & findings
The pilot's improper pre-flight planning, which resulted in an engine failure due to fuel exhaustion.
Factual narrative
On October 7, 2003, at 1900 eastern daylight time, a Cessna 140, N2370N, sustained substantial damaged after a loss of engine power shortly after takeoff from Pace Airport (VA02), Ridgeway, Virginia. The certificated commercial pilot and the passenger were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight conducted under 14 CFR Part 91. The pilot said that he conducted a preflight inspection of the airplane and visually inspected both tanks, which were full. The pilot and the passenger departed on runway 36 and practiced takeoffs and landings. About 35 minutes into the flight, the pilot landed, taxied back to the departure end of the runway, and took off. During climb out, the engine sputtered. The pilot pumped the throttle, and the engine surged momentarily, then stopped producing power completely. He asked the passenger to switch fuel tanks, but the airplane descended rapidly, and collided with trees off the end of the runway. A Federal Aviation Administration (FAA) inspector performed an on-scene examination of the airplane. The inspector said the airplane landed hard on its nose, about 90 degrees vertical, in heavily wooded terrain. Both wings, fuselage, and tail sustained substantial damage. Fuel was noted draining from the right fuel tank filler neck, and the fuel selector handle was set to the left tank. The FAA inspector conducted another examination of the airplane on October 16, 2003, after it had been recovered. According to the inspector, both wings had been removed, but the engine remained attached to the airframe. A temporary fuel system was rigged, and the engine was started. It ran at various power settings, without interruption. The fuel tanks were both breached, and continuity of the fuel system was established. Approximately 1-quart of fuel remained in the left tank, and a substantial amount of fuel remained in the right tank. The airplane was last flown on September 30, 2003, by a private pilot, who was also an airport employee. He said that he departed with full fuel tanks, and flew for 1-hour and 20-minutes, with the fuel selector on the left tank. After the flight, he did not refuel, and placed the airplane in its hangar. The airplane was not flown again until the accident flight. In addition, another pilot, a flight instructor, also stated that this was the airplane's first flight since September 30, 2003. On the day of the accident, the pilot taxied the airplane out of the hangar and proceeded directly to the runway. He did not purchase fuel. The witness did not know if the pilot had conducted a pre-flight inspection. The owner of the airport also confirmed that the airplane had not flown since September 30, 2003. According to the Cessna 140 Operator's Manual, each fuel tank held 12.5 gallons of fuel (10.5 usable), with an average burn rate of 6.5 gallons per hour. The pilot reported a total of 1,130 flight hours, of which 50 were in make and model. Weather at Blue Ridge Airport (MTV), Martinsville, Virginia, about 6 miles northwest, at 1902, was reported as wind calm, visibility 4 statute miles, clear skies, temperature 65 degrees F, dewpoint 60 degrees F, and a barometric pressure setting of 30.16 inches HG. The pilot stated that he had completed a pre-flight inspection, and visually checked both fuel tanks, which were full. However, several witnesses reported that the airplane had been flown for 1-hour and 20-minutes prior to this flight with the fuel selector positioned to the left tank, and was not refueled. On the day of the accident, the pilot departed with the fuel selector still positioned to the left tank, and performed several take-offs and landings. About 35-minutes into the flight, during climb-out, the engine sputtered. The pilot pumped the throttle, and got a momentary gain in engine power, followed by a complete loss of power. He instructed the passenger to switch the fuel selector from the left tank to the right tank, but the airplane descended rapidly into trees. Examination of the airplane revealed that approximately 1-quart of fuel remained in the left tank, and a substantial amount of fuel remained 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_2003_IAD04CA002.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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