NTSB CAROL · Event
Event SEA04LA061
Registry · N5210G
FAA Aircraft Registry record.
Make / Model
CESSNA 305A
Year of manufacture
1951 · 53 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19720113
ADS-B equipped
Yes — Mode-S A68F04
Registrant of record
GRAF III EUGENE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing roll in the tail wheel-equipped aircraft, leading to an inadvertent ground-loop, during which the aircraft's wing impacted the ground.
Factual narrative
On Wednesday, March 31, 2004, approximately 0945 mountain standard time, a Cessna 305A (L-19), N5210G, impacted the terrain during an inadvertent landing roll ground-loop at Bozeman Municipal Airport, Bozeman, Montana. The private pilot, who was the sole occupant, was not injured, but the aircraft, which is owned and operated by a family member of the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which departed Helena, Montana, about 45 minutes earlier, was in visual meteorological conditions at the time of the accident. No flight plan had been filed. There was no report of an ELT activation. According to the pilot, the flare, touchdown, and initial part of the landing roll in the tail wheel-equipped aircraft were normal and uneventful. But as the aircraft slowed, it suddenly swerved to the left, and the pilot's attempts to realign it with the runway were not successful. The aircraft therefore exited the left side of the runway and entered a ground loop. During the ground loop sequence, the right main gear leg partially folded under, and the right wing collided with the terrain. A post accident inspection of the aircraft's braking system, rudder system, and tail wheel did not reveal any evidence of a malfunction or anomaly that would have contributed to a loss of directional control. The flare, touchdown, and initial part of the landing roll in the tail wheel equipped aircraft were normal and uneventful. But as the aircraft slowed, it suddenly swerved to the left, and the pilot's attempts to realign it with the runway were not successful. The aircraft therefore exited the left side of the runway and entered a ground loop. During the ground loop sequence, the right main gear leg partially folded under, and the right wing collided with the terrain. A post accident inspection of the aircraft's braking system, rudder system, and tail wheel did not reveal any evidence of a malfunction or anomaly that would have contributed to a loss of directional control. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_SEA04LA061.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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