What was found
RIGHT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 27 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328403 PT 1. 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 CENTER FLAP RIB 27 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328403 PT 1. MAJOR REPAIR IAW GMM 6-2-100.