As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND ON FUSELAGE EXTERNAL SKIN AT STA 372, STR 32R. A FASTENER IS LOCATED IN THE AFFECTED AREA WHILE IT IS RESTRICTED, PER SRM 53-00-01 ALLOWABLE DAMAGE 1. THE BLEND OUT WAS MEASURED AND FOUND THAT THE NOMINAL THICKNESS IS 0.067" WITH A MINIMUM REMAINING THICKNESS OF 0.064".