NTSB CAROL · Event
Event NYC03CA182
Aircraft involved
Probable cause & findings
The pilot's improper decision to install an inadequate air filter, which subsequently failed and resulted in a power loss.
Factual narrative
On August 23, 2003, about 1430 eastern daylight time, a homebuilt Hyperbipe, N258HB, was substantially damaged following a loss of engine power while departing Marion Municipal Airport, Marion, Ohio. The certificated private pilot and passenger were not injured. Visual meteorological conditions prevailed for the personal flight destined for Beaver County Airport, Beaver Falls, Pennsylvania. No flight plan had been filed for the flight that was conducted under 14 CFR Part 91. The pilot reported that the airplane lost engine power during the initial climb after takeoff. He further stated: "...At approx 250 to 400 feet of altitude, the engine began to loose power slowly. I could not climb or maintain altitude due to the steady loss of power and began to sink rapidly. I picked a field I thought I could make an emergency landing on straight ahead. I pulled the throttle to idle and pulled the mixture to cut off just before touch down as I flared for a landing in a farm field of soy beans. With no injuries to my self or passenger, we exited the plane as quickly as possible...." During a follow-up telephone interview, the pilot reported that from the air, he thought the height of the vegetation in the field he had picked for a landing was about 6 inches; however, it turned out be about 40 inches high. A mechanic who examined the airplane reported that the air filter screen had separated from the support bracket. The filter element was found in the intake to the fuel injection servo and obstructed the air flow to the engine. The mechanic said he had given the airplane a condition inspection about 30 hours before the accident, and an air filter was not installed at that time. The air filter was "home-made" and installed by the pilot. The filter screen was attached to the support bracket by the use of pop rivets. During the initial climb after takeoff, the experimental airplane lost engine power. The pilot performed a forced landing to a field he thought contained vegetation that was about 6 inches high; however, the vegetation was about 40 inches high. During landing, the airplane sustained damage to the lower landing gear structure and lower wings. Examination of the airplane revealed that the air filter screen had separated from the support bracket. The filter element was found in the intake to the fuel injection servo and obstructed the air flow to the engine. The air filter was home-made and installed by the pilot. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_NYC03CA182.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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