As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE WING CENTER SECTION REAR SPAR WEB WAS CRACKED AT APPROX RBL 20.5 AND LBL 11.5. THE CRACK AT RBL 20 IS 2.0 LONG AND A CHEM-MILLED RADIUS JUST BELOW THE SPAR UPPER CHORD. THE CRACK AT LBL 11.5 IS 1.13 LONG ALSO IN THE CHEM-MILLED RADIUS JUST BELOW THE SPAR UPPER CHORD BETWEEN THE STIFFENERS AT LBL 7.5 AND 12.9. REPAIRED PER ERA 362506-14.