NTSB CAROL · Event
Event ERA12LA545
Aircraft involved
Probable cause & findings
A total loss of engine power during the initial climb after takeoff for reasons that could not be determined because examination of the engine did not reveal any anomalies that would have precluded normal operation.
Factual narrative
On September 1, 2012, about 1320 eastern daylight time, a Cessna 172E, N377SP, operated by a private individual, was substantially damaged during a forced landing, after it experienced a total loss of engine power during the initial climb after takeoff from a private airstrip in East Bend, North Carolina. The private pilot and a passenger sustained minor injuries. Visual meteorological conditions prevailed and no flight plan had been filed for the flight destined for the Blue Ridge Airport, Martinsville, Virginia. The personal flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. The pilot reported that he completed an uneventful preflight inspection and engine run-up prior to beginning a takeoff roll from the 2,500-foot-long, turf runway. As the airplane climbed to about 100 feet above the ground, it experienced a total loss of engine power. The pilot was unable to restart the engine. He lowered the nose to avoid a stall, and performed a forced landing to a corn field, which resulted in substantial damage to both wings, the fuselage, and the empennage. The airplane was manufactured in 1964, and was equipped with a Continental O-300-D, 145-horsepower engine. Postaccident examination of the airplane by a Federal Aviation Administration (FAA) inspector did not reveal any mechanical malfunctions that would have precluded normal operation. The airplane’s fuel tanks contained approximately 21 gallons of 100-low-lead aviation gasoline, which was absent of contamination. At the time of the accident, the airplane had been operated for about 19 hours since its most recent annual inspection, which was performed on June 2, 2012. In addition, the engine had been operated for about 1,830 hours since overhaul. The weather reported at airport located about 15 miles east of the accident site included a temperature of 31 degrees Celsius (C) and a dew point of 20 degrees C. Review of an FAA Carburetor Icing Envelope chart placed the reported temperature and dew point in the "serious icing at glide power" area of the chart. The pilot completed an uneventful preflight inspection and engine run-up before takeoff. However, as the airplane climbed to about 100 feet above the ground, it experienced a total loss of engine power. The pilot was unable to restart the engine, so he performed a forced landing to a corn field. Postaccident examination of the airplane did not reveal any mechanical malfunctions that would have precluded normal operation. The airplane’s fuel tanks contained about 21 gallons of uncontaminated aviation gasoline. The airplane had been operated about 19 hours in the 3 months since its most recent annual inspection, and the engine had been operated about 1,830 hours since it was overhauled. Although weather conditions at the time of the accident were conducive to serious carburetor icing at glide power, the investigation was unable to determine the cause of the power loss. 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 Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA12LA545.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 (icing, stall). 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 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other
[Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…
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