DEN03LA046
2003-03-07 · Richfield, Utah, United States · Minor · 1 aircraft · Status: Completed
Airport RIF
Current FAA registration · N8205W
- Make / Model
- PIPER PA-28-180
- Year of manufacture
- 1965 · 38 years old at event
- Engine
- LYCOMING O&VO-360 SER (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19650326
- ADS-B equipped
- Yes — Mode-S AB33F7
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain aircraft control during landing roll resulting in a ground loop/swerve and subsequent nose over. A contributing factor was the gusty wind conditions.
Factual narrative
On March 7, 2003, at approximately 1405 mountain standard time, a Piper PA-28-180, N8205W, owned and operated by the pilot, was substantially damaged when it nosed over during landing roll at Richfield Municipal Airport (RIF), Richfield, Utah. The private pilot, the sole occupant on board, received minor injuries. Visual meteorological conditions prevailed. No flight plan had been filed for this cross-country flight being operated under Title 14 CFR Part 91. The flight originated at Montrose, Colorado, at approximately 1100. According to the pilot's statement, while on the return flight, he received updated weather from an automatic weather observing/reporting system (AWOS). He entered the left downwind for runway 19 at Richfield, and attempted to land. As he began to flare, he encountered a gust of wind from the west. He added power for a go-around and then set up for a landing on runway 01. The touchdown on runway 01 was "normal," but during the landing roll, a gust of wind caught the left wing. He said it "felt like the nose landing gear was skidding across the runway." He attempted to regain control and correct this by adding "full rudder." He thought of applying full power for a go-around, but he felt he was going too slow. The airplane veered off the right side of the runway. After leaving the runway, the nose landing gear "seemed to collapse." The right wing tip struck the ground and the airplane nosed over. The airplane sustained damage to the right wing, vertical stabilizer and rudder. During a telephone interview on March 7, 2003, the pilot stated that the winds were approximately 270 degrees at 12 knots gusting to 28 knots. The pilot was on a return flight and stated that he received an AWOS weather update. He entered the left downwind and attempted to land on 19. As he began to flare, he encountered a gust of wind from the west. He added power for a go-around and then set up for a landing on runway 01. The touchdown on runway 01 was "normal," but during the landing roll, a gust of wind caught the left wing. He said it "felt like the nose landing gear was skidding across the runway." He attempted to regain control and correct this by adding "full rudder." He thought of applying full power for a go-around, but he felt he was going too slow. The airplane veered off the right side of the runway. After leaving the runway, the nose landing gear "seemed to collapse." The right wing tip struck the ground and the airplane nosed over. In a telephone interview, the pilot stated that the winds were approximately 270 degrees at 12 knots gusting to 28 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_DEN03LA046.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (go-around). All research papers
- 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…
- Semantic Scholar 2022 · Article (Journal of Safety Research) Go-around accidents and general aviation safety.
INTRODUCTION Changes in General Aviation (GA) accident rates, specifically in the go-around phase, are examined by comparing the number of accidents, the proportion of fatal accidents, and the proport…
- Semantic Scholar 2021 · Article (Aerospace) Classification and Analysis of Go-Arounds in Commercial Aviation Using ADS-B Data
Go-arounds are a necessary aspect of commercial aviation and are conducted after a landing attempt has been aborted. It is necessary to conduct go-arounds in the safest possible manner, as go-arounds …
- NASA NTRS 2021 · Accepted Manuscript (Version with final changes) Go-Around Criteria Refinement for Transport Category Aircraft
Presently, airline pilots are trained to go around if, when lower than 500 ft above the ground, they are outside of a handful of parameters such as airspeed, position, and rate of descent.
- NASA NTRS 2019 · Conference Paper Validation of Proposed Go-Around Criteria Under Various Environmental Conditions
This paper evaluates the effects of environmental conditions on touchdown performance under varying approach states and validates proposed go-around criteria developed using data from a previously con…