NTSB CAROL · Event
Event IAD02LA097
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed, which resulted in an inadvertent stall/spin. A factor was the airplane's proximity to the ground when the spin commenced.
Factual narrative
On September 29, 2002, about 1615 eastern daylight time, an Aeronca 65-C, N24277, was substantially damaged when it impacted terrain while on a final approach to Front Royal-Warren County Airport (FRR) , Front Royal, Virginia. The certificated private pilot sustained serious injuries. No flight plan was filed for the flight that originated at Deck Airport (9D4), Myerstown, Pennsylvania, about 1400. Visual meteorological conditions prevailed for the personal flight conducted under 14 CFR Part 91. According to the pilot, he made a left downwind entry into the traffic pattern for runway 09. When the airplane was abeam the runway numbers, he retarded the throttle to idle (about 1,000 rpm), and maintained an approach airspeed of 60 knots. Everything was "normal" as the pilot turned the airplane onto the base leg. However, when he was on final approach, the airplane went into a flat spin. The pilot attempted to recover from the spin by adding full power and opposite aileron, but there was not enough altitude remaining, and the airplane hit the ground. The pilot also noted that when he applied full throttle, the engine responded "with plenty of power," and that he "must have passed out for awhile in order to have gotten into this situation." A witness, who was also a private pilot, observed the airplane fly over the airport lower than the traffic pattern altitude. The airplane flew a "normal" left hand traffic pattern, but on final approach, appeared to be "slower than a Cessna 182." Shortly after the airplane was established on final approach, it turned left, flew north, and continued to descend. The left wing and nose of the airplane "dropped", the tail "came up," and the airplane began to spin before it disappeared behind a tree line. The airplane was examined on October 1, 2002. Examination revealed leading edge impact damage and a chordwise fracture of the right wing. The firewall, lower section of fuselage, and the overhead center section were also damaged. The left wing, empennage, and tail control surfaces were not damaged. Control cable continuity was established from all flight control surfaces to the cockpit. The pilot reported a total of approximately 1,000 flight hours, of which, 300 hours were in make and model. He also reported that there were no mechanical deficiencies. Weather at Winchester Regional Airport (OKV), Winchester, Virginia, about 14 nautical miles to the north, at 1619, included winds from 100 degrees at 3 knots, visibility 10 statute miles, and clear skies. The pilot made a left downwind entry into the traffic pattern. When the airplane was abeam the runway numbers, he retarded the throttle to idle, and maintained an approach airspeed of 60 knots. Everything was "normal" as the pilot turned the airplane onto the base leg; however, on final approach, the airplane entered a left spin, and spun to the ground. According to the pilot, there were no mechanical deficiencies with the airplane or engine. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_IAD02LA097.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
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…
Browse the full corpus — academia portal ↗