As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN UNDER DORSAL HAS MINOR CORROSION SPOTS BS 882-893 LBL 6- RBL 5. 8-143. REMOVED MINOR CORROSION ON AREAS IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREAS IAW NDT P4 51-00-00 PROC.3. FOUND WITHIN LIMITS IAW SRM 53-00-01-1A-1 FIG. 103 A-A. TREATED AND PRIMED AREAS IAW SRM-51-21-72-370-801.