What was found
DURING SCHEDULED BRDG CHECK, FOUND WING CENTER SECTION FRONT SPAR STIFFENER SUPPORT ANGLE CRACKED AT BS 540, LBL 57. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED BRDG CHECK, FOUND WING CENTER SECTION FRONT SPAR STIFFENER SUPPORT ANGLE CRACKED AT BS 540, LBL 57. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.