As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
B BELLY DOOR FRAME WITH 1 INCH CRACK AT LT UPPER CORNER AT STA 560.000. PERFORMED MAJOR REPAIR PER SRM 52-20 FIG 2 SHEET 4. STOP DRILLED CRACK PER SRM 52-2-0 FIG 2 SHEET 4. FABRICATED REINFORCING ANGLE PER SRM 52-2-0 FIG 2 SHEET 4. INSTALLED NEW ANGLE PER SRM 52-2-0 FIG 2 SHEET 4 AND SRM 51-1-21 PG 1.