As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PANEL NR 3338 HAS FRETTING CORROSION AROUND EDGE AT MOUNT HOLE. REMOVED CORROSION, ORIGINAL THICKNESS .036". REMOVED .010", .026" REMAINING. MATERIAL IS OUT OF LIMITS REF SRM 53-10-1 PG 1 DETAIL 1. FABRICATED NEW STIFFENER ANGLE 7075-O- .040, HEAT TREATED TO T-6. REF DWG 65-25581, DOCUMENT 65-25581 REV C. TREATED AND PRIMED AND PAINTED. THIS IS CLASSIFIED AS A MINOR REPAIR.