As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND HEAVY CORROSION ON SKIN PANEL BETWEEN FRAME 39-40, STGR 28-33 LT AND TWO OVALIZED HOLES ON FITTING (SEE DRW. A535-10563) AT FRAME 39, STGR 28. REPAIR PERFORMED BY BLEND OUT CORROSION IAW TD 942.038560/011/2005 ISSUE A AND TD 942.038560/047/2005 ISSUE A OVAL HOLES REPAIRED BY OVERSIZING AND BUSHING IAW TD 038560/017/2005 ISSUE B. CONTAINING ALL IN EA 6-5314-82934, APPROVED BY RAS/AS/0153/2005 ISSUE A AND OVERSIZED HOLES WITH RAS/AS/0154/2005 ISSUE A.