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Atlas / NTSB / CHI02LA022

NTSB CAROL · Event

Event CHI02LA022

2001-11-08 Danville, Illinois, United States Airport · DNV None 1 aircraft Status: Completed

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 ↗.