What was found
C11 CHECK - FUSELAGE FLOOR PANEL DELAMINATED BETWEEN FR 53 AND FR 56 AT Y 0. REMOVED AND REPLACED PANEL IAW A321 AMM 53-42-14-000-001-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C11 CHECK - FUSELAGE FLOOR PANEL DELAMINATED BETWEEN FR 53 AND FR 56 AT Y 0. REMOVED AND REPLACED PANEL IAW A321 AMM 53-42-14-000-001-A.