As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FWD O/B FUSELAGE ACCESS PANEL # 193CL HAD BULGING/CRACKED FASTENER HOLES<[01] ALL STEPS COMPLETED.;[02] SUMMARY=PREPARED DAMAGED AREA FOR REPAIR AS MARKED ON PANEL #193CL AS PER B737 SRM 51-70-04-2R-9.<BR>APPLIED REPAIR IN DAMAGED AREA (FASTENER HOLE) ON PANEL #193CL AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED PO#2011230 AND PO#1473815.<BR>APPLIED TOP COAT AS PER AMM 51-21-73-370-803