As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND ANGLE CRACK FROM STA 500D TO STA 520 BL 0<[01] LOCATED AND DRILLED NEW ANGLE SUPPORT BETWEEN FS 500D AND FS 520 BL 0 IN REF SRM 51-40-05-0G-0;[02] STEP #1 ENTER BY ERROR;[03] REMOVED AND INSTALLED NEW ANGLE SUPPORT FROM STA 500D TO STA 520 BL 0 IN REF SRM 51-40-02-0G-0 AND DRAWING NUMBER #143A5400;[04] VERIFIED WORK PERFORMED