NTSB CAROL · Event
Event MIA06CA079
Registry · N4654M
FAA Aircraft Registry record.
Make / Model
MOONEY M20R
Year of manufacture
2005 · 1 years old at event
Engine
CONT MOTOR IO-550 SERIES (300 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20050518
ADS-B equipped
Yes — Mode-S A5AF1E
Registrant of record
CONTRERAS DARRELL WAYNE TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed while attempting a go-around at a low altitude which resulted in an inadvertent stall/mush, an uncontrolled descent and an impact with terrain.
Factual narrative
On April 5, 2006, about 1830 central daylight time, a Mooney M20R airplane, N4654M, registered to and operated by the a private individual, as a Title 14 CFR Part 91 flight, crashed while attempting a go-around following touchdown at Destin, Florida. Visual meteorological conditions prevailed, and an instrument flight rules flight plan had been filed. The private-rated pilot and passenger were not injured, and the airplane incurred substantial damage. The flight originated in Hattiesburg, Mississippi, the same day, about 1730. The pilot stated that about 5 miles from Destin, Florida, he cancelled his IFR flight plan in preparation for the visual approach to runway 14. He said that the winds were from 280 degrees, at a velocity of 10 knots, gusting to 14. At an altitude of 200 feet he said he encountered some turbulence, but made a smooth touchdown on the runway centerline, and after a "couple hundred feet", a strong gust of wind blew him to the left toward the runway edge lights. He said he made the decision to go around, applied full throttle, and "pulled up sharply" to avoid hitting the runway lights. He further stated that the stall warning then activated, so he lowered the nose of the airplane but "apparently did not have sufficient airspeed to maintain altitude. He said he tried to turn back to the runway, but felt a sudden "spin" to the left about 30 degrees, as the airplane impacted the ground. Prior to the accident there were no mechanical failures or malfunctions to the airplane or any of its systems. The pilot stated that he made a smooth touchdown on the runway centerline, and after a "couple hundred feet", a strong gust of wind blew him to the left toward the runway edge lights. He said he made the decision to go around, applied full throttle, and "pulled up sharply" to avoid hitting the runway lights. He further stated that the stall warning then activated, so he lowered the nose of the airplane but "apparently did not have sufficient airspeed to maintain altitude. He said he tried to turn back to the runway, but felt a sudden "spin" to the left about 30 degrees, as the airplane impacted the ground. Prior to the accident there were no mechanical failures or malfunctions to the airplane or any of its systems. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_MIA06CA079.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, go-around, 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.
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- 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…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Low Level Turbulence Detection For Airports
Abstract—— Low level wind shear and turbulence present a serious safety risk to aircraft during the approach, landing and take-off phases.
- Embry-Riddle Scholarly Commons 2018 · Journal article (IJAAA)
Evaluating the Effect of Turbulence on Aircraft During Landing and Take-Off Phases
—— Low level wind shear and turbulence present a serious safety risk to aircraft during the approach, landing and take-off phases.
Browse the full corpus — academia portal ↗