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Atlas / NTSB / DEN02LA058

NTSB CAROL · Event

Event DEN02LA058

2002-06-24 Giddings, Texas, United States Airport · 62H None 1 aircraft Status: Completed

Registry · N83DH

FAA Aircraft Registry record.

Make / Model

AMERICAN CHAMPION AIRCRAFT 8KCAB

Year of manufacture

1997 · 5 years old at event

Engine

LYCOMING AEIO-360 SER (180 hp)

Seats / Engines

1 seats · 1 engine

Last airworthiness date

19970106

ADS-B equipped

Yes — Mode-S AB5654

Registrant of record

HANSEN DOUGLAS M

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the failure of the pilot to maintain aircraft control during the landing rollout. A contributing factor was the subsequent inadvertent ground loop of the airplane.

Factual narrative

On June 24, 2002, at approximately 1100 central daylight time, a American Champion 8KCAB (Decathlon), N83DH, was substantially damaged during a ground loop on landing roll at Giddings-Lee County Airport, Giddings, Texas. The private pilot, the sole occupant on board, was not injured. The pilot/owner was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross-country flight that had originated from Weiser Airpark, Houston, Texas, approximately 45 minutes before the accident. The pilot had not filed a flight plan. The pilot said that he was landing on runway 17, and the airplane suddenly veered "hard" to the right and exited the runway. The left main axle support structure failed, and the left main wheel separated from the airplane. The left strut dug into the ground, and the airplane came to rest on its left wing. The outer 6 feet of the left wing was bent up approximately 35 degrees, and the left side of the elevator was bent. The pilot estimated the wind, at the time of the accident, to be 240 degrees at 3 to 5 knots. The pilot said that he was landing on runway 17, and the airplane suddenly veered "hard" to the right and exited the runway. The left main axle support structure failed, and the left main wheel separated from the airplane. The left strut dug into the ground, and the airplane came to rest on its left wing. The outer 6 feet of the left wing was bent up approximately 35 degrees, and the left side of the elevator was bent. The pilot estimated the wind, at the time of the accident, to be 240 degrees at 3 to 5 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2002_DEN02LA058.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.