NTSB CAROL · Event
Event DEN89LA164
Registry · N82908
FAA Aircraft Registry record.
Make / Model
PIPER PA-32-301T
Year of manufacture
1982 · 7 years old at event
Engine
LYCOMING TI0-540 SER (310 hp)
Seats / Engines
7 seats · 1 engine
Last airworthiness date
19821118
ADS-B equipped
Yes — Mode-S AB54C3
Registrant of record
HALL CHARLES R
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO MAINTAIN AIRCRAFT CONTROL DURING AN ENCOUNTER WITH TURBULENCE. CONTRIBUTING TO THE ACCIDENT WAS THE TURBULENCE.
Factual narrative
THE PRIVATE PLT AND HIS FAMILY, WERE MAKING AN X-COUNTRY FLIGHT. THE PLT REPORTED AN APPROACH TO RWY 27, A 6,900 X 75 FT, ASPHALT RWY, WITH WINDS ESTIMATED FROM 315 DEGREES AT 15 KNOTS. ACCORDING TO THE PLT, THE AIRPLANE ENCOUNTERED A 'GUST FROM BELOW'. THE PLT DESCRIBED LOW LEVEL TURBULENCE AND SAID HE LOST TRACK OF THE AIRSPEED. HE SAID HE HEARD THE STALL HORN AND THE AIRPLANE FELL ABOUT 10 FT TO THE GROUND. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_DEN89LA164.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, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
Browse the full corpus — academia portal ↗