What was found
DURING SCHEDULED 6Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED BETWEEN BS 546 TO BS 560, RBL 32. REMOVED AND REPLACED ANGLE PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 6Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED BETWEEN BS 546 TO BS 560, RBL 32. REMOVED AND REPLACED ANGLE PER SRM.