CHI91LA279
1991-09-01 · DECATUR, Illinois, United States · None · 1 aircraft · Status: Completed
Airport DEC
N686EE has since been reassigned. It is now registered to a different aircraft (SONEX AIRCRAFT ONEX, built 2018), which was not involved in this event.
Aircraft involved
Probable cause & findings
INADEQUATE PREFLIGHT PLANNING AND PREPARATION AND AIRPLANE PERFORMANCE DATA NOT UNDERSTOOD BY THE PILOT. FACTORS ASSOCIATED WITH THE ACCIDENT ARE THE PILOT'S LACK OF TOTAL EXPERIENCE IN TYPE OF OPERATION, DELAYED REMEDIAL ACTION, AND THE OPERATOR'S INSUFFICIENT STANDARDS AND REQUIREMENTS.
Factual narrative
THE ACCIDENT AIRPLANE COLLIDED WITH TREES AND TERRAIN WHILE ATTEMPTING TO CLIMB FROM TAKEOFF WITH A SAILPLANE IN TOW. THE SAILPLANE RELEASED FROM THE TOW PLANE AND RETURNED TO THE DEPARTURE AIRPORT. ACCORDING TO THE PILOT THE AIRPLANE ENCOUNTERED LIGHT TO MODERATE TURBULENCE DURING INITIAL CLIMB AND THE AIRPLANE SANK INTO TREES ONE MILE NORTH OF THE AIRPORT. IN AN INTERVIEW AFTER THE ACCIDENT THE PILOT DID NOT REMEMBER DOING A WEIGHT AND BALANCE CALCULATION BEFORE TAKEOFF. WHEN QUESTIONED ABOUT STALL RECOGNITION AND RECOVERY THE PILOT STATED THAT THE ACCIDENT AIRPLANE WAS DIFFERENT FROM OTHER AIRCRAFT IN THAT YOU ONLY HAD TO HOLD THE NOSE UP AND THE AIRPLANE WOULD FLY ITSELF OUT. THE DENSITY ALTITUDE AT THE TIME OF THE ACCIDENT WAS 2500 FEET. THE AIRPLANE WAS ESTIMATED TO BE AT OR SLIGHTLY ABOVE ALLOWABLE GROSS WEIGHT AT TAKEOFF. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_CHI91LA279.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, turbulence). All research papers
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
- arXiv 2026 · arXiv preprint Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- 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 2025 · arXiv preprint Explainable LiDAR 3D Point Cloud Segmentation and Clustering for Detecting Airplane-Generated Wind Turbulence
Wake vortices - strong, coherent air turbulences created by aircraft - pose a significant risk to aviation safety and therefore require accurate and reliable detection methods.