ASN Wikibase Occurrence # 356756
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Date: | Sunday 1 September 1996 |
Time: | 15:05 LT |
Type: | Piper PA-28-161 |
Owner/operator: | Vernair |
Registration: | N4366Y |
MSN: | 28-8416053 |
Year of manufacture: | 1984 |
Total airframe hrs: | 8453 hours |
Engine model: | Lycoming O-320-D3G |
Fatalities: | Fatalities: 0 / Occupants: 3 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Skwentna, AK -
United States of America
|
Phase: | En route |
Nature: | Unknown |
Departure airport: | Anchorage, AK (MRI) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot & 2 passengers departed on a local area sightseeing flight. While in cruise flight at about 4,000 ft, the engine developed a vibration, then lost power. Oil spray was deposited on the windshield. The pilot performed an emergency landing on a sand bar. After landing, he noticed that the entire propeller, propeller flange, & the outboard end of the engine crankshaft were missing from the engine. Examination of the engine revealed evidence of fatigue cracking, emanating from a corrosion pit on the inner diameter surface of the crankshaft bore. Numerous other corrosion pits were found adjacent to the fracture origin. The engine manufacturer reported the engine was built & shipped from the factory on 4/13/81. The engine was the subject of a mandatory service bulletin (S/B), dated 1018/94, that addressed the inspection of the inside bore of the crankshaft for the presence of corrosion. The S/B required that an initial inspection be conducted within the next 200 hrs of operation or 1 year from the date of the S/B. The operator's company manual stated the Director of Maintenance shall ensure that current manufacturer's mandatory S/B's were complied with. No record of compliance with the S/B was noted in the engine maintenance records.
Probable Cause: corrosion and subsequent fatigue failure of the crankshaft, which resulted in engine failure and a forced landing. Factors related to the accident were: the lack of suitable terrain for a forced landing, and the operator's non-compliance with a service bulletin.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | ANC96LA140 |
Status: | Investigation completed |
Duration: | 1 year and 7 months |
Download report: | Final report |
|
Sources:
NTSB ANC96LA140
Location
Revision history:
Date/time | Contributor | Updates |
13-Mar-2024 10:36 |
ASN Update Bot |
Added |
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