Accident Air Tractor AT-401 N4542W,
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ASN Wikibase Occurrence # 290403
 
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Date:Tuesday 19 August 2014
Time:07:40 LT
Type:Silhouette image of generic AT3P model; specific model in this crash may look slightly different    
Air Tractor AT-401
Owner/operator:Aurora Cooperative
Registration: N4542W
MSN: 401-0767
Year of manufacture:1989
Total airframe hrs:7969 hours
Engine model:Pratt & Whitney R-1340-S3H1G
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Wray, Colorado -   United States of America
Phase: Initial climb
Nature:Agricultural
Departure airport:Wray, CO (2V5)
Destination airport:Wray, CO (2V5)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
During initial climb, the pilot felt a subtle vibration from the engine and noticed the manifold pressure dropping rapidly. When he attempted to increase manifold pressure by opening the throttle, the engine began to vibrate violently and lost all power. The pilot made a downwind forced landing, and the airplane nosed over. The engine was later partially disassembled and examined. A small amount of aluminum and steel filings were recovered from oil drained from the rocker arm sump. A cylinder compression check revealed that the Nos. 1 and 3 cylinders were non-functioning and that the No. 4 cylinder exhibited weak compression. The intake valve in the No. 3 cylinder was found to have a ridge worn on its face, and the valve seat was worn excessively. The No. 1 cylinder's exhaust valve was stuck open and was binding in the valve guide. The exhaust valve clearances for the cylinders were then checked and found to be less than the Pratt and Whitney overhaul limits of 0.003" to 0.0055", with a maximum wear limit of 0.010". Most likely, the engine lost power due to the stuck exhaust valve.

Probable Cause: A loss of the No. 1 cylinder's compression due to a stuck exhaust valve caused by a lack of sufficient valve clearance, which resulted in a loss of engine power and a forced landing. Contributing to the loss of engine power were the worn intake and exhaust valves in cylinders No. 3 and 4.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN14LA439
Status: Investigation completed
Duration: 5 months
Download report: Final report

Sources:

NTSB CEN14LA439

Location

Revision history:

Date/timeContributorUpdates
06-Oct-2022 14:42 ASN Update Bot Added

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