As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STA 920 FRAME CHORD HAS 2 BROKEN OUT AREAS LOCATED UNDER THE 1ST AND 3RD LOCK FASTENERS BELOW THE CLIP AT S10R. DAMAGE IS SEEN ON AFT SIDE OF FRAME. REMOVED DAMAGED SECTION IAW SRM 51-70-12. FABRICATED REPAIR ANGLES, FILLER IAW SRM 51-70-12. LOCATED, DRILLED AND DEBURRED PARTS IAW SRM 51-40-05. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED REPAIR PARTS PER SRM 51-70-12.