20011108030549A

Accident · No damage

FAA accident report · Smith AEROSTAR 601 · Danville, IL · November 8, 2001

Date
November 8, 2001 · 11:45 local
Place
Danville, IL
Airport
Vermilion County
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N128AC
NTSB investigation
NTSBCHI02LA022

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On November 8, 2001, about 11:45 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 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. (.19) on November 8, 2001, about 1200 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 FL ight 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 assemely was found broken loose from the upper mounting collar on the landing gear strut and the lower strut was rotated about 90 degrees.

As the FAA filed it

(-23) ON NOVEMBER 8, 2001, ABOUT 11:45 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 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. (.19) ON NOVEMBER 8, 2001, ABOUT 1200 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 FL IGHT 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 ASSEMELY WAS FOUND BROKEN LOOSE FROM THE UPPER MOUNTING COLLAR ON THE LANDING GEAR STRUT AND THE LOWER STRUT WAS ROTATED ABOUT 90 DEGREES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N128AC · 1

Matched to the same aircraft by N-number and date.