As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1.5 INCH CRACK RT SIDE CANTED FRAME. STOP-DRILLED 1.5" CRACK PER SRM 53-01. ACCOMPLISHED HFEC CRACK CONTAINED IAW SRM 53-01. FABRICATED DOUBLER PER SRM 53-01 FIG 2. ALODINED PER SRM 53-10-3. PRIMED PER PROCESS STANDARD MANUAL 900-3-6 NR 3. INSTALLED DOUBLER PER SRM 53-01. RESTORED FINISH PER PS 900-3.