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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 ↗.

Related research

Matched on aircraft type or causal vocabulary (go-around). All research papers