What was found
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT RIVET HOLES DUE TO CORROSION BULGING SKIN AT BS 1011 AND O/T B/D AND INBD SIDE OF STR 26L. REPAIRED PER BOEING SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT RIVET HOLES DUE TO CORROSION BULGING SKIN AT BS 1011 AND O/T B/D AND INBD SIDE OF STR 26L. REPAIRED PER BOEING SRM.