ASN Wikibase Occurrence # 358311
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| Date: | Monday 4 September 1995 |
| Time: | 12:05 LT |
| Type: |  Stinson 108-1 |
| Owner/operator: | Private |
| Registration: | N8865K |
| MSN: | 108-1865 |
| Total airframe hrs: | 1294 hours |
| Engine model: | FRANKLIN 6A4-165-BC |
| Fatalities: | Fatalities: 0 / Occupants: 3 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Corvallis, OR -
 United States of America
|
| Phase: | Landing |
| Nature: | Private |
| Departure airport: | (KCVO) |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
AFTER DEPARTING RUNWAY 17 THE PILOT REMAINED IN THE PATTERN FOR A TOUCH-AND-GO. UPON TOUCHDOWN AT 70 MPH, ON CENTERLINE, THE RIGHT MAIN LANDING GEAR COLLAPSED. POSTCRASH EXAMINATION REVEALED THAT THE FOUR RETAINING PINS WHICH HOLD THE RIGHT MAIN LANDING GEAR SHOCK STRUT RETAINER CAP HAD SHEARED ALLOWING THE STRUT TO SEPARATE FROM THE GEAR STRUT. NO PRE-EXISTING FATIGUE WAS OBSERVED ON THE PINS. THE AIRCRAFT HAD BEEN GROUND-LOOPED 14.3 HOURS PREVIOUS TO THIS ACCIDENT.
Probable Cause: SHEARING OF THE RIGHT MAIN LANDING GEAR SHOCK STRUT RETAINER CAP RETAINING PINS.
Accident investigation:
 |
|
Sources:
NTSB SEA95LA204
History of this aircraft
Other occurrences involving this aircraft
| 20 June 2000 | N8865K | Private | 0 | MOUNTAIN HOME, Idaho | |
sub |
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 14-Mar-2024 12:07 | ASN Update Bot | Added |
Corrections or additions? ... Edit this accident description
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