What was found
LEFT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 11 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 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.
LEFT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 11 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT1. MAJOR REPAIR IAW GMM 6-2-100.