HOUSTON, MS, USA
N21ER
CESSNA 172N
DURING NORMAL CRUISE FLT A PORTION OF ONE PROPELLER BLADE SEPARATED. THE PLT LANDED THE ACFT IN A FIELD & DURING THE LANDING ROLL, THE ACFT COLLIDED WITH A HAYSTACK. EXAMINATION OF THE PROPELLER BLADE REVEALED IT SEPARATED AT BLADE STATION 28.5. METALLURGICAL EXAMINATION REVEALED IT FAILED DUE TO FATIGUE FROM A NICK IN THE LEADING EDGE OF THE BLADE.
Source: NTSB Aviation Accident Database
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