- Date
- November 8, 2001, 11:45 local (17:45 UTC)
- Place
- Danville, IL
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N128ACSmith Aerostar 601
- Weather
- Visual (VMC) · Day
- Status
- Completed · report July 15, 2002
- Report
- Approved by Office Director
- Parties
- FAA-Springfield, Illinois-FSDO
- FAA report
- 20011108030549A
- Case key
- 53738
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
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.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
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.
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.
Aircraft
- Registration
- N128AC
- Reported as
- Smith Aerostar 601
- Category
- Airplane
- Serial number
- 61-0170-084
- Airframe hours
- 4,452
- Engines
- Lycoming IO-540, 290 horsepower, reciprocatingLycoming IO-540, 290 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Positioning · Part 91
- Operator
- Name
- Registered owner
- George J. Camarata
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · October 20, 2001 · 5 hours before
- Departed
- MKE · Milwaukee, WI
- Destination
- DNV · Danville, IL
- Flight plan
- IFR
- Airport
- DNV · Vermilion County, runway 34, 3,999 × 100 ft, asphalt
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 48
- Injuries
- None
- Certificate
- Commercial
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Last flight review
- July 30, 2001
- Seat
- Left
- Flight hours
- 4,500 total · 980 in this make and model · 4,250 as pilot in command · 120 in the last 90 days · 50 in the last 30 days · 3 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 290° at 13 knots
- Visibility
- 5 statute miles
- Lowest ceiling
- 1,800 ft
- Temperature
- 57 °F, dew point 52 °F
- Altimeter
- 30.18 inHg
- Observed at
- DNV
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.