What was found
ONE INCH CRACK LOCATED AT UPPER PART OF DRIVE PULLEY FRAME STRUT ASSEMBLY. CRACK ORIGINATED AT WELD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ONE INCH CRACK LOCATED AT UPPER PART OF DRIVE PULLEY FRAME STRUT ASSEMBLY. CRACK ORIGINATED AT WELD.