Accident Beechcraft F33A Bonanza N80WH,
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ASN Wikibase Occurrence # 228459
 
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Date:Friday 23 August 2019
Time:08:46 LT
Type:Silhouette image of generic BE33 model; specific model in this crash may look slightly different    
Beechcraft F33A Bonanza
Owner/operator:Magnolias Pride Inc
Registration: N80WH
MSN: CE-504
Year of manufacture:1974
Total airframe hrs:4674 hours
Engine model:Continental IO-550B
Fatalities:Fatalities: 0 / Occupants: 3
Aircraft damage: Substantial
Category:Accident
Location:Hobe Sound, Martin County, FL -   United States of America
Phase: En route
Nature:Private
Departure airport:Stuart-Witham Field, FL (SUA/KSUA)
Destination airport:Stuart-Witham Field, FL (SUA/KSUA)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
During low-altitude cruise flight, the engine lost total power and the pilot performed a forced landing on an embankment next to a road, resulting in substantial damage to the right wing, right tip tank, and right elevator. Postaccident examination of the engine revealed that the crankshaft was fractured between the No. 2 main bearing journal and the No. 2 connecting rod journal and exhibited evidence of lubrication distress. Additionally, the No. 2 bearing had shifted, and a large portion of the bearing had extruded from the bearing support. The bearing support mating surfaces displayed fretting and the lock tab had completely worn away. Based on the observed damage, it is likely that the No. 2 main bearing shifted, resulting in inadequate lubrication to, and subsequent failure of, the crankshaft.

While the crankcase mating surfaces displayed unapproved sealant material with no signs of silk thread, which was not consistent with the engine manufacturer's guidance for engine assembly, the breakaway through bolt torque remained at or above the manufacturer's specification. It could not be definitively determined, based on available evidence, if the use of an unapproved sealant contributed to the bearing shift.

Probable Cause: A bearing shift, which resulted in a loss of lubrication to the crankshaft, the failure of the crankshaft, and a total loss of engine power.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA19LA258
Status: Investigation completed
Duration: 2 years and 8 months
Download report: Final report

Sources:

NTSB ERA19LA258
FAA register: https://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=80WH

Location

Revision history:

Date/timeContributorUpdates
24-Aug-2019 01:27 Geno Added
24-Aug-2019 03:53 RobertMB Updated [Location, Phase, Nature, Source, Damage, Narrative]
24-Aug-2019 21:49 Captain Adam Updated [Narrative]
01-Jul-2022 19:20 ASN Update Bot Updated [Time, Other fatalities, Destination airport, Source, Damage, Narrative, Category, Accident report]

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