Probable cause
The failure of the right main landing gear due to a preexisting crack adjacent to a weld line.
NTSB analysis
The pilot reported that the approach was “on speed,” but upon initial touchdown the airplane bounced. The airplane then landed “firm” and immediately veered off the runway surface. Structural damage to the fuselage resulted. An inspector from the Federal Aviation Administration (FAA) reported that a section of the right main landing gear structure had failed. Postaccident examination of the fracture surface, which was adjacent to a weld line, revealed evidence of a preexisting crack. There was differential rusting on the crack surface indicative of progressive crack extension. The airplane had recently undergone an annual inspection, however the FAA inspector reported that the fracture surface could not be seen without disassembly of the landing gear.
Text from the NTSB. Open the NTSB docket for ERA09LA467 for the full record.
Event
- Date
- Aug 17, 2009
- Type
- Accident
- Place
- White Plains, New York
- Nearest airport
- Westchester County (HPN)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Cessna 140A
- N-number
- N9467A
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.