As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MULTIPLE AREAS OF CORROSION ON UPPER FUSELAGE SKIN UNDER DORSAL FIN; BS 847-1007; S-2L TO S-2R ; / [01] REMOVED CORROSION ON EXTERNAL FUSELAGE SKIN BS908-BS1000 BETWEEN STR3L-STR3R WL308 I.A.W SRM 51-10-02-0G-0;SRM 53-00-01-1A-1 PAR 4.A(2)(A) FIG.103/ALLOWABLE DAMAGE 1 DETAILS C;D [16] VERIFIED DAMAGED AREAS OF SKIN UNDER DORSAL FIN; BS 847-1007; REPAIRED ON EA 21-153-03562 AND EA 21-153-03562-WIP1