NTSB CAROL · Event
Event DEN03LA106
Registry · N9221C
FAA Aircraft Registry record.
Make / Model
CESSNA 180
Year of manufacture
1955 · 48 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560215
ADS-B equipped
Yes — Mode-S ACC816
Registrant of record
CRUSON MICHELLE E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's inadequate compensation for wind conditions and his failure to maintain directional control.
Factual narrative
On June 15, 2003, at 1932 mountain daylight time, a Cessna 180, N9221C, was substantially damaged when it ground looped during the landing roll at Ogden-Hinckley Airport (OGD), Ogden, Utah. The private pilot and passenger were not injured. Visual meteorological conditions prevailed and no flight plan had been filed. The flight was conducted under the provisions of Title 14 CFR Part 91. The cross-country flight originated in Provo, Utah, at 1840. According to the pilot, he was landing on runway 25 "with a gusty crosswind component." During the roll-out, the airplane began to "track right and off [the] runway." Subsequently, the airplane departed the right side of the runway and ground looped. Post accident examination revealed a bent left wing, a collapsed left main landing gear, and a crushed gearbox and bulkhead. An examination of the airplane's systems revealed no anomalies. At 1953 the OGD METAR (routine aviation weather report), winds were 330 degrees at 8 knots. According to the pilot operating handbook, the Cessna 180 has a 12 knot maximum demonstrated crosswind component. The crosswind component was calculated to be 8 knots. The pilot was landing on runway 25 "with a gusty crosswind component." During the roll-out, the airplane began to "track right and off [the] runway." The airplane departed the right side of the runway and ground looped. The reported winds were 330 degrees at 8 knots. According to the pilot operating handbook, the Cessna 180 has a 12 knot maximum demonstrated crosswind component. The crosswind component was calculated to be 8 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_DEN03LA106.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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- arXiv 2024 · arXiv preprint
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- arXiv 2024 · arXiv preprint
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- Embry-Riddle Scholarly Commons 2024 · Conference paper
Integrated Propulsion and Control of Rotorcraft
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- NASA NTRS 2023 · Presentation
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- Embry-Riddle Scholarly Commons 2023 · Conference paper
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