What was found
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 548, LBL 54. 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 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 548, LBL 54. REMOVED AND REPLACED ANGLE PER SRM.