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Richmond, CA
The student had recorded her primary flight lesson on a tape recorder. After reaching the practice area, the CFI instructed the student to turn 180 deg left. The student complied and performed a shallow bank turn. Seconds later, while cruising at 2,200 ft, the CFI began talking. In midsentence an undetermined event occurred which interrupted his speech. A wind-like background noise started, and the student exclaimed 'help.' Radar data confirmed witness reports that the tail boom and M/R had separated in level flight. Examination of the wreckage indicated mast bumping had occurred, a M/R blade crushed the left side of the inboard tail cone, and the entire mast with attached M/R blades broke out of the top of the transmission. The outboard tail boom and rotor assembly have not been found. Evidence of a main rotor blade divergence was found. Spectrum analysis of the tape revealed no anomalies until the CFI's voice was terminated. Within 2 seconds the rotor speed appeared to significantly oscillate and abruptly end.
A DIVERGENCE OF THE MAIN ROTOR FROM ITS NORMAL PLANE OF ROTATION FOR AN UNDETERMINED REASON(S) WHICH RESULTED IN ROTOR CONTACT TO THE TAILBOOM.
THE STUDENT HAD RECORDED HER PRIMARY FLIGHT LESSON ON A TAPE RECORDER. AFTER REACHING THE PRACTICE AREA, THE CFI INSTRUCTED THE STUDENT TO TURN 180 DEG LEFT. THE STUDENT COMPLIED AND PERFORMED A SHALLOW BANK TURN. SECONDS LATER, WHILE CRUISING AT 2,200 FT, THE CFI BEGAN TALKING. IN MIDSENTENCE AN UNDETERMINED EVENT OCCURRED WHICH INTERRUPTED HIS SPEECH. A WIND-LIKE BACKGROUND NOISE STARTED, AND THE STUDENT EXCLAIMED 'HELP.' RADAR DATA CONFIRMED WITNESS REPORTS THAT THE TAIL BOOM AND M/R HAD SEPARATED IN LEVEL FLT. EXAM OF THE WRECKAGE INDICATED MAST BUMPING HAD OCCURRED, A M/R BLADE CRUSHED THE LEFT SIDE OF THE INBOARD TAIL CONE, AND THE ENTIRE MAST WITH ATTACHED M/R BLADES BROKE OUT OF THE TOP OF THE TRANSMISSION. THE OUTBOARD TAIL BOOM AND ROTOR ASSEMBLY HAVE NOT BEEN FOUND. EVIDENCE OF A MAIN ROTOR BLADE DIVERGENCE WAS FOUND. SPECTRUM ANALYSIS OF THE TAPE REVEALED NO ANOMALIES UNTIL THE CFI'S VOICE WAS TERMINATED. WITHIN 2 SECONDS THE ROTOR SPEED APPEARED TO SIGNIFICANTLY OSCILLATE AND ABRUPTLY END.