ATL03LA045
2003-02-12 · Bolivar, Tennessee, United States · Minor · 1 aircraft · Status: Completed
Airport M08
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons. A factor was trees.
Factual narrative
On February 12, 2003, at 2120 central standard time, a Cessna P210N, N6ZZ, registered to a private owner and operated by a commercial pilot reported an in-flight emergency due to an engine failure while enroute to Memphis International Airport, Memphis, Tennessee. The pilot made a forced landing onto unsuitable terrain. The personal flight was conducted under the provisions of Title 14 CFR Part 91 with an instrument flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The pilot and the passenger received minor injuries, and the airplane was destroyed. The flight originated from Greenville Downtown Airport, Greenville, South Carolina on February 12, 2003, eastern standard time, at 1848. According to the pilot during cruise flight at 6000 feet, the engine power began to decrease. The pilot checked the quantity of the fuel tanks, and fuel was present. According to the pilot the engine continued to run but was not producing full power. Repeated efforts by the pilot to restore full engine power failed. The pilot radioed Memphis Approach control, and reported an in-flight emergency due to an engine failure. The controller issued the pilot radar vectors to William L. Whitehurst Field, Bolivar, Tennessee. The airplane collided with trees in a heavily wooded area 5 miles south of the airport, and there was a post-crash fire. Examination of the airplane revealed the airplane was heavily fire damaged. Examination of the engine was conducted at Teledyne Continental Motors, Inc. on October 29, 2003, with FAA and NTSB representatives present. There were no abnormalities discovered during the examination of the engine. According to the pilot during cruise flight at 6000 feet, the engine power began to decrease. The engine continued to run but was not producing full power. Repeated efforts by the pilot to restore full engine power failed. The pilot radioed Memphis Approach control, and reported an in-flight emergency due to an engine failure. The controller issued the pilot radar vectors to William L. Whitehurst Field, Bolivar, Tennessee. The airplane collided with trees five miles south of the airport. Examination of the airplane revealed that it was heavily fire damaged. There were no abnormalities discovered during the examination of the engine. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_ATL03LA045.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 (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…