As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION CHECK, CORROSION WAS FOUND ON LOWER SKIN STA 208-270 LONGERON 32RH-32 LT. CORROSION WAS REMOVED IAW SRM 51-1-8 PAGE 20, THICKNESS WAS MEASURED IAW ASTME 79701 AND IT WAS FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE2P. SKIN WAS REPLACED IAW DRAWING 5613862, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-2-1 FIGURE 4 TR 53-172 AND EWO ATI 53-028.