NTSB CAROL · Event
Event NYC03LA109
Aircraft involved
Probable cause & findings
A partial loss of engine power for undetermined reasons.
Factual narrative
On May 19, 2003, about 1220 eastern daylight time, a Cessna 175A, N6989E, was substantially damaged while ditching in the Atlantic Ocean, following a loss of engine power after takeoff from Ocean City Municipal Airport (26N), Ocean City, New Jersey. The certificated commercial pilot was not injured. Visual meteorological conditions prevailed for the planned flight to Cape May County Airport (WWD), Wildwood, New Jersey. No flight plan was filed for the personal flight conducted under 14 CFR Part 91. The pilot reported that during the initial climb, about 800 feet msl, the engine experienced a partial loss of power. The pilot made a 180-degree turn back toward the airport, but was unable to maintain altitude. He ditched the airplane in shallow water near the coast, about 2 miles south of the airport. The pilot further stated that it was possible that the airplane's single fuel vent was obstructed, which resulted in the power loss. Examination of the wreckage by a Federal Aviation Administration (FAA) inspector revealed damage to the left wing and fuselage. He also observed fuel in both fuel tanks. The inspector stated that he examined fuel vent and did not find any blockage. The FAA inspector, with assistance of an aircraft recovery company, drained water from the carburetor. He also drained and replaced the engine oil; removed, cleaned, and reinstalled all spark plugs; and rotated the crankshaft. The inspector attained thumb compression on all cylinders and confirmed crankshaft, camshaft, and valve train continuity. However, the engine would not start. Subsequently, the carburetor was inspected and no discrepancies were noted. Both magnetos were inspected, and the left magneto was subsequently cleaned. On the second attempted, the engine "fired," but did not run. The inspector could not determine why the engine experienced a partial loss of power. During the initial climb, about 800 feet msl, the engine experienced a partial loss of power. The pilot made a 180-degree turn back toward the airport, but was unable to maintain altitude. He ditched the airplane in shallow water about 2 miles south of the airport. The pilot stated that it was possible that the airplane's single fuel vent was obstructed, which resulted in the power loss. Examination of the wreckage revealed that both fuel tanks contained fuel, and the fuel vent was not blocked. Examination of the engine did not reveal any pre-impact mechanical malfunctions. Thumb compression and valve train continuity were obtained, and the engine initially started. However, it did not continue to run. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_NYC03LA109.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 (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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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