Hard landing Accident North American Navion A N969TR,
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ASN Wikibase Occurrence # 216049
 
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Date:Friday 5 October 2018
Time:14:45
Type:Silhouette image of generic NAVI model; specific model in this crash may look slightly different    
North American Navion A
Owner/operator:Private
Registration: N969TR
MSN: NAV-4-342
Year of manufacture:1946
Total airframe hrs:3336 hours
Engine model:Continental E-225-4
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Clarke County, MS -   United States of America
Phase: En route
Nature:Private
Departure airport:Meridian-Key Field, MS (MEI/KMEI)
Destination airport:Gulf Shores-Edwards Airport, AL (GUF/KJKA)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot stated that, while en route to his destination, the airplane's engine sputtered and then lost total power. During the subsequent forced landing to a highway, the airplane landed hard, and the landing gear collapsed; the airplane sustained substantial damage to the fuselage. A postaccident examination of the engine revealed the No. 3 cylinder exhaust valve fractured where the stem transitioned to the valve head seat. The valve head impacted the No. 3 piston and became lodged between the crankcase and the camshaft, which resulted in the fracture of the camshaft. Fatigue cracking, which initiated at multiple sites, propagated through the valve stem. The presence of a tapered stem near the fracture surface, high temperature oxide deposits, and fatigue striations on the fracture surface suggested that the stem underwent spallation or erosion of the oxides formed during high temperature exposure, which would reduce the stem cross-section over time, increasing the likelihood of initiating fatigue cracking. Additionally, a localized area of wear on the top face of the valve stem was most likely due to the valve not rotating during operation, which could create hot spots or improper thermal dissipation in the hottest parts of the valve and lead to valve damage or failure.

Probable Cause: The fatigue failure of the No. 3 cylinder exhaust valve, which resulted in a fractured camshaft and a total loss of engine power.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA19LA008
Status: Investigation completed
Duration: 1 year and 10 months
Download report: Final report

Sources:

NTSB

Location

Images:


Photo: NTSB

Media:

Revision history:

Date/timeContributorUpdates
06-Oct-2018 00:18 Geno Added
06-Oct-2018 10:00 Iceman 29 Updated [Time, Phase, Nature, Departure airport, Destination airport, Source, Embed code]
07-Oct-2018 19:16 harro Updated [Departure airport, Destination airport, Embed code]
15-Aug-2020 16:00 ASN Update Bot Updated [Time, Departure airport, Destination airport, Source, Narrative, Accident report, ]
15-Aug-2020 16:25 harro Updated [Departure airport, Destination airport, Source, Narrative, Photo, Accident report, ]

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