NTSB CAROL · Event
Event CHI01LA061
Registry · N2184N
FAA Aircraft Registry record.
Make / Model
MOONEY M20S
Year of manufacture
1999 · 2 years old at event
Engine
CONT MOTOR IO-550 SERIES (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19991027
ADS-B equipped
Yes — Mode-S A1DA2B
Registrant of record
PLANE CONVENIENT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot failed to maintain directional control of the airplane and the runway selected resulted in a tailwind condition. Factors associated with the accident were the gusty crosswind and the snow bank.
Factual narrative
On January 1, 2001, at 1245 eastern standard time, a Mooney M20S, N2184N, operated by a private pilot collided with a snow bank while landing on runway 04 (5,103 feet by 100 feet) at the St. Clair County International Airport, Port Huron, Michigan. The pilot was not injured and the airplane was substantially damaged. The 14 CFR Part 91 flight was operating in visual meteorological conditions without a flight plan. The flight originated from Detroit, Michigan, at 1200 eastern standard time. The pilot reported he flew a practice ILS approach to runway 04. The approach was terminated in a go-around followed by VFR traffic pattern and full stop landing on runway 04. He reported the winds were out of the northwest at 10 knots. He then departed on runway 04 and made a left hand traffic pattern for another landing. The pilot reported, "Final approach required minimal crab to correct for crosswind and then mild slip to maintain the centerline." He reported that just prior to touchdown while 2 feet above the runway "…a significant gust ballooned the aircraft 5-6 ft. above the runway where the aircraft stalled and began to settle abruptly with a nose high attitude." He reported he applied power to recover, but could not gain enough airspeed. The airplane veered to the right and the right main landing gear contacted the snow on the side of the runway. According to the pilot, the airplane spun around clockwise into the snow where it came to rest. The local weather observation, taken 5 minutes prior to the accident, reported winds from 270 degrees at 11 knots, gusting to 18 knots. The airplane contacted a snow bank on the side of the runway during landing. The landing was being made on runway 04 (5,103 feet by 100 feet). The pilot reported the winds were from the northwest at 10 knots and that a "minimal" crosswind correction was required on final approach. He continued to report that just prior to touchdown while 2 feet above the runway "…a significant gust ballooned the aircraft 5-6 ft. above the runway where the aircraft stalled and began to settle abruptly with a nose high attitude." The pilot added power in an attempt to recover, however, the airplane traveled to the right side of the runway where it contacted a snow bank and spun around prior to coming to rest. The local weather observation, taken 5 minutes prior to the accident, reported winds from 270 degrees at 11 knots, gusting to 18 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_CHI01LA061.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). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
Browse the full corpus — academia portal ↗