What was found
INSPECTION FOUND ONE INCH CRACK AFTER STRESS RELIEF AND FPI, WELDED STRUT IAW 72-54-01 RU02 REPAIR C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND ONE INCH CRACK AFTER STRESS RELIEF AND FPI, WELDED STRUT IAW 72-54-01 RU02 REPAIR C.