As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME BS 301 HAS CORROSION ON FUSELAGE SKIN CLIP BETWEEN STRS 31 AND 32 LT. REMOVED LIGHT CORROSION ON FUSELAGE SKIN CLIP BETWEEN STR 31 & 32LT AT FS X301.00, REF SRM 51-21-00, PROCEDURE A 1 AND 2 NO MATERIAL LOSS NOTED. RESTORED FINISH ON FUSELAGE SKIN CLIP BETWEEN STR 31 & 32 LT AT FS X301.00, REF SRM 51-20-00.