Incident Details
During a routine instructional flight, one blade of the fixed pitch propeller separated approximately three feet from the hub. The resulting imbalance caused a broken engine mount and a total loss of power. The pilot executed a forced landing in a soft field, during which the aircraft nosed over.
Investigation Findings
A metallurgical examination of the failed blade, designated design number 1A103, revealed a fatigue crack. The crack originated from chordwise surface scratches located underneath the painted finish. The propeller had accumulated 3,425 total service hours since new and had not been refinished during that time.