As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FORWARD FUSELAGE SKIN HAD CORROSION AND A PREVIOUS REPAIR THAT WAS NOT IAW THE SRM, FROM FS 218 TO 256 AND BETWEEN LONGERON'S 14 AND 16 RIGHT. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10849-MR.