Incident Piper PA-28R-200 Arrow N4350T,
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ASN Wikibase Occurrence # 146445
 
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Date:Monday 18 June 2012
Time:10:45
Type:Silhouette image of generic P28R model; specific model in this crash may look slightly different    
Piper PA-28R-200 Arrow
Owner/operator:Marshall County Flying Club Inc
Registration: N4350T
MSN: 28R-7235014
Year of manufacture:1971
Total airframe hrs:5697 hours
Engine model:Lycoming IO-360-C1C
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Minor
Category:Incident
Location:Marshall County Airport - C75, Lacon, IL -   United States of America
Phase: En route
Nature:Private
Departure airport:Lacon, IL (C75)
Destination airport:Lacon, IL (C75)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that he was flying the airplane at 4,500 feet mean sea level with 23 inches of manifold pressure and with the engine at 2,350 to 2,400 rpm when the airplane began to abnormally vibrate. He scanned the instruments and observed no other abnormal indications. He executed an emergency landing to an airport without incident. The examination of the airplane revealed that about 6 inches of a propeller blade tip had separated from the propeller. The metallurgical examination of the fracture surface revealed that a fatigue crack had originated about 0.06 inch from the blade’s leading edge. A surface gouge was found at the origin of the fatigue crack, which indicated that the direction of the damage was from the leading to trailing edge consistent with foreign object impact to a rotating propeller. A test of the airplane’s tachometer revealed that it was indicating 50 rpm higher than the actual propeller rpm and that it had a restricted propeller operating range from 2,100 to 2,350 rpm. When the pilot set the propeller to 2,350 or 2,400 rpm using the airplane’s tachometer, the actual rpm would have been operating within the restricted rpm range.

Probable Cause: The propeller blade’s failure due to a fatigue crack that originated from a surface gouge that resulted from foreign object damage to the propeller blade that occurred at an unknown time.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN12IA377
Status: Investigation completed
Duration: 2 years 1 month
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
22-Jun-2012 23:51 Geno Added
23-Jun-2012 00:23 Alpine Flight Updated [Time, Damage]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
28-Nov-2017 20:17 ASN Update Bot Updated [Other fatalities, Departure airport, Destination airport, Source, Narrative]

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