Wirestrike Accident Cessna 210-5 (205) N8464K,
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ASN Wikibase Occurrence # 202110
 
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Date:Friday 2 April 1999
Time:15:25 LT
Type:Silhouette image of generic C205 model; specific model in this crash may look slightly different    
Cessna 210-5 (205)
Owner/operator:Zosel, Paul, J.
Registration: N8464K
MSN: 2050460
Total airframe hrs:4398 hours
Engine model:Continental IO-470-S
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Edison, WA -   United States of America
Phase: En route
Nature:Private
Departure airport:Bellingham, WA (KBLI)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
Shortly after takeoff, and while cruising at 3,000 feet (mean sea level) over Samish Bay, the Cessna 205's Continental IO-470-S engine ceased developing power. With the propeller continuing to windmill, and only muddy fields available, the pilot initiated a forced landing to a north/south paved road at the south end of the bay. The pilot, observing power lines along the west side of the road, landed along the east side. During the landing roll the left wing impacted a sign. With the pilot being unable to maintain directional control of the aircraft following the sign impact, the aircraft departed the left side of the road into a deep ditch. Post-crash examination of the engine revealed that the crankshaft had separated at the number six cheek. Metallurgical examination of the crankshaft revealed that a large area in the central portion of number six cheek fracture surface displayed a smooth texture and contained multiple crack arrest features, characteristic of fatigue progression originating at the outboard flat surface of the crankcheek, approximately at the mid point between the horizontal centerlines for the main and rod journals. No further determination could be made regarding the initiating condition of the fatigue due to post-separation heat and mechanical damage to the fracture features.

Probable Cause: A total loss of engine power due to fatigue of the number six crankcheek resulting in crankshaft separation, and the lack of suitable terrain. Contributing factors were the sign and the ditch.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: SEA99LA046
Status: Investigation completed
Duration: 12 months
Download report: Final report

Sources:

NTSB SEA99LA046

Location

Revision history:

Date/timeContributorUpdates
26-Nov-2017 12:38 ASN Update Bot Added
08-Apr-2024 07:48 ASN Update Bot Updated [Time, Operator, Other fatalities, Phase, Departure airport, Source, Narrative, Category, Accident report]

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