NTSB CAROL · Event
Event CEN13CA389
Aircraft involved
Probable cause & findings
The failure of both the flight instructor and the pilot to monitor and manage the fuel on board, which resulted in an engine failure due to fuel starvation.
Factual narrative
The pilot and flight instructor had been flying for over two hours, doing air work and making touch-and-go landings at Bridgeport (XBP), Alliance-Fort Worth (AFW), Meacham (FTW) and Hicks Airports (T67). Returning to XBP, they were making a final touch-and-go landing when the engine lost power. Unable to glide back to the runway, the flight instructor made a forced landing in a plowed field north of the airport. The airplane touched down hard, shearing off the landing gear, and sliding 60 feet before coming to a stop. The firewall was buckled. The flight instructor and pilot sustained minor injuries. A Federal Aviation Administration (FAA) inspector examined the airplane and reported the fuel selector was positioned on the left fuel tank. When electrical power was applied, the left fuel gauge registered empty. One quart of fuel was drained from the left fuel tank. The right fuel tank had not been compromised and contained fuel. The pilot and flight instructor were making touch-and-go landings when the engine lost power. Unable to glide to the runway, they made a forced landing in an open field. During the forced landing, the landing gear was sheared off and the firewall was buckled. The student sustained a serious injury and the flight instructor received minor injuries. A Federal Aviation Administration inspector examined the airplane and reported the fuel selector was positioned on the left fuel tank. When electrical power was applied, the left fuel gauge registered empty. No fuel was observed in the left fuel tank. The right fuel tank had not been compromised and contained fuel. 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).
- C Personnel issues-Action/decision-Action-Forgotten action/omission-Pilot - C
- C Personnel issues-Action/decision-Action-Forgotten action/omission-Instructor/check pilot - C
- C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management - C
Verbatim from NTSB's published report. Source file
NTSB_2013_CEN13CA389.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 ↗