TUCKERTON, NJ, USA
N1072G
BELL 206L-1
ACCORDING TO THE PLT AT 8 TO 10 FT IN A HOVER THE CYCLIC SNAPPED REARWARD 3 TO 4 IN WITH A NOISE FROM THE REAR. THE TAILBOOM WAS FOUND BENT APRX 45 DEGREES DOWN AND 15 DEGREES RIGHT WITH NO EVIDENCE OF GROUND CONTACT ON THE TAIL SKID SHOE. METALLURGICAL ANALYSIS INDICATED COMPRESSIVE BUCKLING DAMAGE CONSISTENT WITH EXCESSIVE BENDING LOADS ON THE BOOM. INSPECTION OF THE HELICOPTER DID NOT REVEAL ANY MECHANICAL FAILURES/MALFUNCTIONS.
Source: NTSB Aviation Accident Database
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