As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE FWD PRESSURE BULKHEAD PANEL HAS A WEB REPAIR ON RIGHT SIDE AT STA 1156 BETWEEN 39 TO 42 DIM 12 X 18 INCHES, 20 X 28 INCHES, 20 X 28 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.