As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R-1 DOOR FUSELAGE CUTOUT, AFT LOWER CORNER HAD .5 INCH CRACK IN CENTER OF RADIUS. STOP DRILLED CRACK AND OPENED HOLE TO .250 IAW 53-10-01. HFEC PART IAW 737 SRM 51-00-00 FIG 20, FABRICATED DOUBLER AND TRIPLER FRM (2024T3 .063 QQA 250-5 R699111) AND INSTALLED IAW 737 SRM 53-10-01.