NTSB CAROL · Event
Event ANC04LA023
Registry · N226P
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SF50
Year of manufacture
2024
Engine
WILLIAMS FJ33-5A
Seats / Engines
7 seats · 1 engine
Last airworthiness date
20241222
ADS-B equipped
Yes — Mode-S A1F890
Registrant of record
CLRMET MT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for a crosswind condition during landing, which resulted in a loss of control and an on-ground encounter with terrain. Factors associated with the accident were a crosswind, and an inadvertent ground loop.
Factual narrative
On February 14, 2004, about 1338 eastern standard time, a wheel-equipped Piper PA-18-160 airplane, N226P, sustained substantial damage during a loss of control and subsequent ground loop during landing at the Naples Airport, Naples, Florida. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight under Title 14, CFR Part 91, when the accident occurred. The private certificated pilot, and the one passenger, were not injured. Visual meteorological conditions prevailed. The flight originated at the Marathon Airport, Marathon, Florida, about 1215. No flight plan was filed, nor was one required. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on February 17, 2004, the pilot reported that he was landing on runway 23, which required a correction for a strong left crosswind. The pilot stated that at touchdown, a strong gust of wind lifted the left wing, and the airplane subsequently ground looped to the right. During the ground loop, the right wing and right aileron struck the surface of the runway and sustained structural damage. At 1338, an Aviation Routine Weather Report (METAR) for the Naples Airport was reporting, in part: wind, 180 degrees (true) at 15 knots, peak gusts 22 knots; visibility, 10 statute miles; clouds and sky condition, few at 1,500 feet; temperature, 81 degrees F; dew point, 70 degrees F; altimeter, 29.95 inHg. The pilot noted that there were no preaccident mechanical anomalies with the airplane. The private certificated pilot reported that he was landing on runway 23, which required a correction for a left crosswind. The pilot stated that at touchdown, a strong gust of wind lifted the left wing, and the airplane subsequently ground looped to the right. During the ground loop, the right wing and right aileron struck the surface of the runway and sustained structural damage. At 1338, an Aviation Routine Weather Report (METAR) was reporting the wind as 180 degrees (true) at 15 knots, with peak gusts of 22 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_ANC04LA023.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 (loss of control). 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 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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