NTSB CAROL · Event
Event CHI02LA022
Registry · N128AC
FAA Aircraft Registry record.
Make / Model
SMITH AEROSTAR 601
Year of manufacture
1974 · 27 years old at event
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19811112
ADS-B equipped
Yes — Mode-S A0716D
Registrant of record
CGA HOLDINGS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The separation of the main landing gear scissor assembly during landing for undetermined reasons, resulting in the directional control of the airplane not being possible.
Factual narrative
On November 8, 2001, about 1145 central standard time, a Smith Aerostar 601, N128AC, piloted by a commercial pilot, sustained substantial damage during landing on runway 34 (3,999 feet by 100 feet, asphalt) at the Vermillion County Airport, Danville, Illinois. The 14 CFR Part 91 positioning flight was on an instrument flight rules flight plan and was operating in visual meteorological conditions. The pilot, who was the sole occupant, was not injured. The flight originated from the General Mitchell International Airport, Milwaukee, Wisconsin, about 1045. The pilot reported that during the landing, he heard a loud noise and the airplane veered off of the runway. Upon inspection, the landing gear scissor assembly was found broken loose from the upper mounting collar on the landing gear strut and the lower strut was rotated about 90 degrees. A request was made that the broken parts be sent to the National Transportation Safety Board investigator for further examination. As of March 8, 2002, the parts had not been received. No other anomalies were found with the airplane or its systems that could be associated with a pre-impact condition. The airplane veered off of the runway during landing. The pilot reported that during the landing, he heard a loud noise and then the airplane veered off of the runway. Upon inspection, the landing gear scissor assembly was found broken loose from the upper mounting collar on the landing gear strut and the lower strut was rotated about 90 degrees. A request was made that the broken parts be sent to the National Transportation Safety Board investigator for further examination. The parts were not received. No other anomalies were found with the airplane or its systems that could be associated with a pre-impact condition. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_CHI02LA022.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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