Service difficulty report · Blade · Hiller UH12D

Difficulty date
August 14, 2005
Submitted
June 6, 2006
Operation
General aviation
Make and model
Hiller UH12D
Aircraft time
15,187 hours
Part
Blade
Part number
2253110104
Condition
Failed
Location
Main Rotor
Part time
6,594 hours
Stage of operation
DE
How discovered
O
Nature of condition
E
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

A SEVERE VERT VIBRATION OCCURRED WHEN HELICOPTER ENTERED A SPRAY RUN. VIBRATION CEASED JUST BEFORE LANDING ON A NEARBY ROAD. ROTOR HEAD WAS REMOVED AND NDT'D FOR CRACKS, NONE FOUND. HELICOPTER WAS RE-ASSEMBLED, ALL FLT CONTROLS WERE CHECKED FOR DAMAGE AND SECURITY, AND TEST FLOWN OK UNTIL AUTO-ROTATION WAS ENTERED. VERT VIBRATION RE-OCCURRED, BUT DISAPPEARED WHEN POWER APPLIED. MAIN ROTOR BLADES WERE CHECKED AND ADJUSTED FOR TRACK AND BALANCE AND NEXT FLT, VERT VIBRATION DEVELOPED WHILE UNDER PWR, AT APPROX 40 KNOTS IAS. HELICOPTER IMMEDIATELY LANDED ON THE ROAD BELOW, WITH A TAILROTOR STRIKE RESULTING. HIGH TIME MAIN ROTOR BLADES HAVE BEEN RETIRED AND TAILROTOR SUDDEN STOPPAGE INSPECT IN PROGRESS.

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