What was found
S2 CHECK - CABIN FLOOR PANEL 232DG HAS AREA OF DISBOND BETWEEN FR 26.1 AND FR 31 AT -Y1975. REPAIRED CABIN FLOOR PANEL 232DG BETWEEN FR 26.1 AND FR 31 AT -Y1975 IAW A330 AMM 25-28-43.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
S2 CHECK - CABIN FLOOR PANEL 232DG HAS AREA OF DISBOND BETWEEN FR 26.1 AND FR 31 AT -Y1975. REPAIRED CABIN FLOOR PANEL 232DG BETWEEN FR 26.1 AND FR 31 AT -Y1975 IAW A330 AMM 25-28-43.