As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT AND RIGHT FORWARD JACKING SUPPORT ANGLES ARE CORRODED. BLEND SUPPORT ANGLES IAW SRM 51-42-06-001-001 & 51-21-06-001-001. PERFORMED UT THICKNESS OF BLEND AREAS IAW MAC NDT INSPECTION PROCEDURE UT-3. MINIMUM MATERIAL REMAINING LT .060", RT .061", ORIGINAL IS .063" MATERIAL REMOVED IS .003". REPAIRED IAW REO 670-53-11-689, STEP 1.