What was found
(AUS) TAIL ROTOR BLADE LEADING EDGE EROSION STRIP SEPARATED FROM BLADE CAUSING HIGH FREQUENCY VIBRATION - SUSPECT CAUSED BY DEFECTIVE BOND BETWEEN BLADE LEADING EDGE AND EROSION STRIP
- Difficulty date
- July 22, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Snias SA330J
- Engine
- Tmeca TURMO4C
- System (JASC)
- 6410 · Tail Rotor Blades
- Part
- Blade
- Part number
- 330A12000534
- Condition
- Faulty
- Location
- Tail Rotor Blade
- Stage of operation
- CL
- Nature of condition
- E
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.