What was found
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, RBL 41.5. REMOVED AND REPLACED STIFFENER PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, RBL 41.5. REMOVED AND REPLACED STIFFENER PER SRM.