As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE ACCESS PANEL 193B LOWER SKIN SURFACE HAS SEVERAL ELONGATED HOLES.<[01] APPLIED REPAIR. AT PANEL 193B PER B737 SRM 53-40-70-2R-1 ; B737 SRM<BR>51-70-04-2R-9 AND B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7 & 4.N.2) TOOL USED TEMPERATURE CONTROL ID 160354 DUE DATE 02-16-24; VACUUM GAGE ID 173239 DUE DATE 02-23-24. MATERIAL USED RESIN 9390 PO# 1791128 AND FIBER GLASS PO#1738579; APPLIED TOPCOAT ON LOWER FUSELAGE ACCESS PANEL 193B LOWER SKIN REF B 737 AMM 51-21-73-370-803;[02] VERIFIED CORRECTIVE ACTION.