Narrative:

During shallow climb following several practice emergency approachs to a dry lakebed; the engine started vibrating badly. A 180 degree turn was initiated back to the lake while a scan of the instruments indicated the engine was producing power normally. Once landing on lakebed was assured; propeller was pulled to low RPM and engine was shut down. Dead stick landing followed without further difficulty or damage/injury. Inspection of aircraft revealed the loss of approximately 4 inches of 1 propeller blade. No evidence of bird strike or other impact damage is apparent. Propeller manufacturer has been contacted; propeller section will be provided for analysis. Callback conversation with reporter revealed the following information: postflt revealed that a propeller tip had separated in-flight causing the vibration. The aircraft is routinely operated from dirt strips. However there was no visible damage to the propeller that could have caused the tip to fail. The blade has been returned to the manufacturer and is currently undergoing engineering analysis.

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Original NASA ASRS Text

Title: PLT RPTS ENG VIBRATION ON CLBOUT AFTER PRACTICE EMER LNDG ON DRY LAKE BED. ACFT IS RETURNED FOR AN ACTUAL EMER LNDG ON THE DRY LAKE.

Narrative: DURING SHALLOW CLB FOLLOWING SEVERAL PRACTICE EMER APCHS TO A DRY LAKEBED; THE ENG STARTED VIBRATING BADLY. A 180 DEG TURN WAS INITIATED BACK TO THE LAKE WHILE A SCAN OF THE INSTS INDICATED THE ENG WAS PRODUCING PWR NORMALLY. ONCE LNDG ON LAKEBED WAS ASSURED; PROP WAS PULLED TO LOW RPM AND ENG WAS SHUT DOWN. DEAD STICK LNDG FOLLOWED WITHOUT FURTHER DIFFICULTY OR DAMAGE/INJURY. INSPECTION OF ACFT REVEALED THE LOSS OF APPROX 4 INCHES OF 1 PROP BLADE. NO EVIDENCE OF BIRD STRIKE OR OTHER IMPACT DAMAGE IS APPARENT. PROP MANUFACTURER HAS BEEN CONTACTED; PROP SECTION WILL BE PROVIDED FOR ANALYSIS. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: POSTFLT REVEALED THAT A PROP TIP HAD SEPARATED INFLT CAUSING THE VIBRATION. THE ACFT IS ROUTINELY OPERATED FROM DIRT STRIPS. HOWEVER THERE WAS NO VISIBLE DAMAGE TO THE PROP THAT COULD HAVE CAUSED THE TIP TO FAIL. THE BLADE HAS BEEN RETURNED TO THE MANUFACTURER AND IS CURRENTLY UNDERGOING ENGINEERING ANALYSIS.

Data retrieved from NASA's ASRS site as of January 2009 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.