As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CHAFFED FS 96900-FS 985.00 STR 27. COMPLIED WITH EC TC REO 670-53-00-290 REV D DATED 09-10-2015 AS WRITTEN. PERFORMED UT THICKNESS INSPECTION IAW BSC NDT INSPECTION PROCEDURE 4.3, MIN MATERIAL REMAINING IS .091", ORIGINAL IS .188", REMOVED IS .027". PERFORMED EDDY CURRENT INSPECTION IAW NDTM PART 1, 51-20-006-250-A01. NO INDICATIONS NOTED AT THIS TIME.