What was found
DURING ROUTINE INSPECTION, MAIN ROTOR BLADE SN:A-4318 EROSION STRIP HAS DELAMINATION EXTENDING 1.75 INCHES BY 1.3 INCHES FROM OUTBOARD TIP OF BLADE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, MAIN ROTOR BLADE SN:A-4318 EROSION STRIP HAS DELAMINATION EXTENDING 1.75 INCHES BY 1.3 INCHES FROM OUTBOARD TIP OF BLADE.