Probable cause
The collapse of the left main landing gear truss due to a weld joint failure, which resulted in substantial damage to the fuselage frame structure.
NTSB analysis
The father of the passenger reported that his son, who was the passenger and owner, had just purchased the airplane, that a prepurchase inspection was conducted, and that “everything looked good.” The pilot was conducting a personal, local flight in the airplane, which included normal maneuvers and several touch-and-go landings with no issues. However, after the last landing and while taxiing the airplane back to the ramp, the left main landing gear (MLG) collapsed.
Examination of the left MLG’s truss structure, which is welded to the fuselage, revealed substantial damage to the fuselage frame structure. Examination also revealed that a weld joint where the truss mounts to the fuselage was cracked and broken. Rust was noted around the weld area, and it appeared that a previous crack had been repaired. The father reported that the area of the failure was hidden behind the bungee and was not visible during the prepurchase inspection. Given the evidence, it is likely that the left main landing gear collapsed due to the weld joint failure.
Text from the NTSB. Open the NTSB docket for WPR16LA174 for the full record.
Event
- Date
- Aug 24, 2016
- Type
- Accident
- Place
- Corvallis, Oregon
- Nearest airport
- Corvallis Muni (CVO)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Amateur-built SC SKYBOLT
- N-number
- N300SB
- Category
- Airplane
- Year built
- 1993
- 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.