Pilot Debrief

PIPER PA 28 near Lone Pine, CA — 2014-09-15

Final reportWPR14LA377
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Date
2014-09-15
Location
Lone Pine, CA, USA
Aircraft
PIPER PA 28
Registration
N5948W
Category
Airplane
Highest injury
Serious
Fatalities
0
Phase of flight
Cruise

Probable cause

The fatigue failure of a propeller blade due to a propeller strike by/of an unidentified object at an unknown time.

NTSB narrative

The private pilot reported that, 2 hours into the personal cross-country flight, he observed a "flash of something" depart the front of the airplane and that the airplane instantly began violently shuddering and vibrating. The pilot immediately landed the airplane in a clearing, and he observed that almost half of one of the propeller blades was missing. A postaccident examination of the propeller assembly revealed that the propeller blade was fractured about 24 inches from the blade butt. Examination of the fracture surface revealed characteristics of fatigue failure that originated in a stress raiser located about 1.25 inches from the leading edge on the lower blade surface. A witness mark, in the form of a distinct score line, was present, indicating that the blade experienced a strike, which created a flaw of critical size at the fatigue origin site that ultimately propagated to failure. The investigation could not determine whether an object struck the blade or the blade struck an object or when the strike occurred.

Analysis

Primary failure mode
Mechanical failure
First missed decision gate
Pilot could have conducted a more thorough preflight inspection of the propeller.

NTSB coding

Evidence available

  • Photos
  • 7 docket documents
View NTSB final reportView NTSB docket

Docket documents7

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