What was found
RIGHT WING FLAPS INTERNAL STRUCTURE, FOUND OUTER FLAP RIB 3 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0328395 PT1 MAJOR REPAIR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING FLAPS INTERNAL STRUCTURE, FOUND OUTER FLAP RIB 3 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0328395 PT1 MAJOR REPAIR IAW GMM 6-2-100.