ERA14CA040
2013-11-05 · Blountville, Tennessee, United States · None · 1 aircraft · Status: Completed
Airport TRI
Aircraft involved
Probable cause & findings
The pilot's delayed reaction and loss of directional control while performing a simulated engine failure during the takeoff roll. A factor in the accident was the CFI's delayed reaction to the loss of directional control.
Factual narrative
According to the pilot and the certificated flight instructor (CFI), the intent of the flight was a proficiency check required by the pilot's insurance carrier, and that the accident occurred while performing a simulated engine failure during the takeoff roll. The pilot reported that after the CFI retarded the power on an engine, the airplane veered to the right. As the airplane exited the edge of the runway he attempted to ground loop it in order to avoid an antenna that was directly in their path. The CFI reported that the pilot "delayed in retarding the power." The CFI subsequently retarded both mixtures, in an attempt to stop the airplane. The airplane subsequently impacted an antenna, which resulted in substantial damage to the fuselage of the airplane. The CFI reported no abnormities with the airplane prior to the accident. According to the pilot and the certificated flight instructor (CFI), the intent of the flight was a proficiency check required by the pilot's insurance carrier, and that the accident occurred while performing a simulated engine failure during the takeoff roll. The pilot reported that after the CFI retarded the power on an engine, the airplane veered to the right. As the airplane exited the edge of the runway he attempted to ground loop it in order to avoid an antenna that was directly in their path. The CFI reported that the pilot "delayed in retarding the power." The CFI subsequently retarded both mixtures, in an attempt to stop the airplane. The airplane subsequently impacted an antenna, which resulted in substantial damage to the fuselage of the airplane. The CFI reported no abnormities with the airplane prior to the accident. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Action/decision-Action-Delayed action-Pilot - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- F Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - F
- — Environmental issues-Physical environment-Object/animal/substance-Tower/antenna (incl guy wires)-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA14CA040.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- 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…