NTSB CAROL · Event
Event IAD96LA049
Aircraft involved
Probable cause & findings
a partial loss of engine power due to spark plug failure, and the pilot's evasive maneuver to avoid lights at the end of the runway.
Factual narrative
On March 14, 1996, at 1615 eastern standard time, a Kitfox IV-1200, N32495, impacted the runway shortly after takeoff at Hummel Field, in Saluda, Virginia. The certificated private pilot reported no injuries, and the one passenger received minor injuries. The airplane sustained substantial damage. Visual meteorological conditions prevailed at the time of the accident, no flight plan was filed. The local flight was conducted under 14 CFR Part 91. The pilot stated that as the airplane climbed through about 50 feet above the ground after takeoff, there was a partial loss of engine power. He stated that the airplane would not climb, so he elected to land on the remaining runway. The pilot reported that he knew that the airplane would touch down very near the end of the runway, and he was concerned about hitting the lights at the end of the runway. He stated that in his attempt to avoid the lights at the end of the runway, he "...ran out of airspeed... ." He reported that the airplane stalled at approximately ten feet above the surface, impacted the runway in a steep nose down attitude, then "...rolled over onto it's back." A post accident inspection of the aircraft by Federal Aviation Administration (FAA) safety inspectors included an electrical function test under compression load for each of the four engine spark plugs. The number one spark plug in the number one cylinder failed this test. No other mechanical anomalies were noted. The pilot's written statement indicated that the spark plug operated normally under low load conditions, but "...[stopped] under full load. [This] was not detected on run up or liftoff." The pilot stated that there was a partial loss of engine power shortly after the airplane lifted off. The airplane would not climb, so he elected to land on the remaining runway. In his attempt to avoid lights at the end of the runway, the pilot stalled the airplane approximately ten feet above the surface. The airplane impacted the runway in a steep nose down attitude, then '...rolled over onto it's back.' Postaccident investigation revealed that the #1 spark plug failed an electrical function test. The pilot stated that the spark plug operated normally under low load conditions, but '...[stopped] under full load.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_IAD96LA049.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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