NTSB CAROL · Event
Event ATL02LA132
Registry · N2044X
FAA Aircraft Registry record.
Make / Model
CESSNA 182H
Year of manufacture
1965 · 37 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19650227
ADS-B equipped
Yes — Mode-S A1A3D9
Registrant of record
NC FLYERS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilots improper flare, during an attempted landing.
Factual narrative
On June 4, 2002, at 1700 eastern standard time, a Cessna 182, N2044X, had a hard landing on touch down at Saint Paul private airstrip, North Carolina. The airplane was registered to and owned by the private pilot. The personal flight was operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological condition prevailed at the time of the accident. The airplane sustained substantial damage, and the private pilot was not injured. The flight originated from Hilton Head, South Carolina, at 1730. The airplane was on short final when the pilot noticed that the airspeed was low. The stall warning horn began to sound approximately 50 feet above the ground. The pilot stated he pitched the nose down and had the flaps extended in the full down position. The pilot did not add any power, but continued the approach without changing the configuration. After clearing the trees approximately 4 to 5 feet over the threshold, the pilot rotated for the flare, the nose dropped and the nose wheel impacted the runway. The airplane bounced and control was established by adding power. The airplane landed on the main landing gear on the second touchdown. During a post accident examination of the airplane, stringers on the copilot's side were found damaged. Further examination revealed the firewall was also buckled. No mechanical problems were reported by the pilot. Examination of the airplane did not reveal any flight control or mechanical problems. The flight was on short final when the pilot noticed that the airspeed was low. During the landing flare, the nose dropped and the nose wheel impacted the runway. No mechanical problems were reported by the pilot. Examination of the airplane did not reveal any flight control or mechanical problems. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_ATL02LA132.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). 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 …
- 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…
Browse the full corpus — academia portal ↗