What was found
DURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERIOR FUSELAGE SKIN AT BS 500 AND STR 26L. FUSELAGE SKIN WAS ROUTED OUT AND REPAIRED IN ACCORDANCE WITH ENGINEERING AUTHORIZATION EA 53-737-185, SRM 53-00-01 AND SRM 53-30-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERIOR FUSELAGE SKIN AT BS 500 AND STR 26L. FUSELAGE SKIN WAS ROUTED OUT AND REPAIRED IN ACCORDANCE WITH ENGINEERING AUTHORIZATION EA 53-737-185, SRM 53-00-01 AND SRM 53-30-03.