What was found
MAIN ROTOR BLADE HAS CRACK LOCATED ON THE TOP SIDE, 104 1/8 INCHES OUTBOARD OF THE BLADE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN ROTOR BLADE HAS CRACK LOCATED ON THE TOP SIDE, 104 1/8 INCHES OUTBOARD OF THE BLADE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.