NTSB CAROL · Event
Event DEN07CA023
Registry · N87VF
FAA Aircraft Registry record.
Make / Model
AMERICAN CHAMPION AIRCRAFT 7GCBC
Year of manufacture
2007
Engine
SUPERIOR O-360 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20070630
ADS-B equipped
Yes — Mode-S ABF5DE
Registrant of record
AGRI FLITE INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain directional control during the landing roll, and his failure to maintain airspeed which resulted in a stall and hard landing.
Factual narrative
On November 13, 2006, at 0938 mountain standard time, an American Champion 7GCBC, N87VF, piloted by a commercial pilot, was substantially damaged when it landed hard during an attempted an aborted landing at Santa Fe Municipal Airport (SAF), Santa Fe, New Mexico. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The pilot and passenger on board the airplane were not injured. The local flight originated from Santa Fe approximately 0700. The pilot said he made a normal wheel landing and allowed the tail to settle. When the tail wheel touched the runway, the airplane veered sharply to the left. The pilot applied full right rudder but the airplane did not respond. The airplane departed the left side of the runway and the pilot applied full power in an attempt to abort the landing. The airplane lifted off briefly, then "settled back on the runway, impacted, and spun around." The FAA inspector who went to the scene said his investigation revealed that during the landing abort, the airplane lifted off, stalled, and landed hard. Post-accident inspection revealed the left wing spar was bent, and a rib was broken, the left elevator and rudder were bent, the empennage was twisted, and the left main landing gear was torn off. Flight control continuity was established, and no system anomalies were found. The pilot made a normal wheel landing and allowed the tail to settle. When the tail wheel touched the runway, the airplane veered sharply to the left. The pilot applied full right rudder but the airplane did not respond. The airplane departed the left side of the runway and the pilot applied full power in an attempt to abort the landing. The airplane lifted off, stalled, and landed hard. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_DEN07CA023.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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