Accident Piper PA-28-180 Cherokee C N8364W,
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ASN Wikibase Occurrence # 69798
 
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Date:Monday 2 November 2009
Time:14:03
Type:Silhouette image of generic P28A model; specific model in this crash may look slightly different    
Piper PA-28-180 Cherokee C
Owner/operator:Private
Registration: N8364W
MSN: 28-2559
Year of manufacture:1965
Engine model:Lycoming O-360-A3A
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Coldwater, Michigan -   United States of America
Phase: En route
Nature:Private
Departure airport:Pontiac, MI (PTK)
Destination airport:Champagne, IL (CMI)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that he was in cruise flight at 2,500 feet above mean sea level when the engine oil temperatures started to rise. He started to divert to a nearby airport, but the engine seized and he executed a forced landing to a field. The inspection of the engine revealed a hole in the crankcase at the #4 cylinder position. The #4 piston connecting rod was found disconnected from the crankshaft, and it was deformed and bent into a “U” shape. The #4 connecting rod cap was separated from the #4 connecting rod. One of the connecting rod bolts was found sheared in half with the nut still attached to one end of the bolt. The other connecting rod bolt was not located in the connecting rod or in the rod cap. A connecting rod bolt was found in the bottom of the engine. The bolt threads exhibited some impact damage, but otherwise, the connecting rod bolt was intact and was not bent. The nut for the connecting rod bolt was not located in the engine. The engine logbook indicated that four new pistons were installed on May 31, 2003. The logbook entry did not indicate that the connecting rods had been replaced. On May 1, 2007, the #4 cylinder was replaced, but there was no indication in the logbook entry that the #4 piston or connecting rod had been repaired or replaced.
Probable Cause: A loss of engine power due to the separation of the No. 4 piston connecting rod as a result of inadequate torque of the connecting rod bolt.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN10LA037
Status: Investigation completed
Duration: 8 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
03-Nov-2009 08:44 Geno Added
03-Nov-2009 09:29 RobertMB Updated
21-Dec-2016 19:25 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
02-Dec-2017 17:49 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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