CHI06CA180
2006-07-03 · Jefferson City, Missouri, United States · None · 1 aircraft · Status: Completed
Airport JEF
Current FAA registration · N43060
- Make / Model
- PIPER PA-28-161
- Year of manufacture
- 1983 · 23 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19830418
- ADS-B equipped
- Yes — Mode-S A52661
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The dual student's excessive landing flare and his failure to maintain adequate airspeed, which resulted in the airplane stalling. A factor to the accident was the flight instructor's delayed remedial action and the runway edge light that the airplane struck.
Factual narrative
The airplane impacted a 24-inch high runway edge light during landing. The flight instructor reported that during the landing flare the student "over flared, causing the airplane to stall" and that the airplane drifted to the right side of the runway. The flight instructor stated that he then assumed aircraft control and "applied full throttle and leveled the wings," but the airplane "settled for a moment before gaining speed and altitude." The flight instructor reported that he "felt and heard" the airplane impact the runway light while he was regaining aircraft control. The flight instructor stated that he flew the airplane back to the runway centerline and landed without further incident. The airplane impacted a 24-inch high runway edge light during landing. The flight instructor reported that during the landing flare the student "over flared, causing the airplane to stall" and that the airplane drifted to the right side of the runway. The flight instructor stated that he then assumed aircraft control and "applied full throttle and leveled the wings," but the airplane "settled for a moment before gaining speed and altitude." The flight instructor reported that he "felt and heard" the airplane impact the runway light while he was regaining aircraft control. The flight instructor stated that he flew the airplane back to the runway centerline and landed without further incident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_CHI06CA180.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
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- Pilots of America Community ↗
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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…