What was found
MAIN CABIN FLOOR PANEL 81 CHAFED THROUGH AT FASTENER HOLE, FWD END. INSTALLED REPAIR DOUBLER AQUIRING MAT IAW DC9 53-23-0 .025 7075T6 PO 1120200 FABED. REPAIR IAW SRM 53-01, TREATED & PRIMED IAW SRM 51-10-3S. REQUIRED INSP COMPLETED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR PANEL 81 CHAFED THROUGH AT FASTENER HOLE, FWD END. INSTALLED REPAIR DOUBLER AQUIRING MAT IAW DC9 53-23-0 .025 7075T6 PO 1120200 FABED. REPAIR IAW SRM 53-01, TREATED & PRIMED IAW SRM 51-10-3S. REQUIRED INSP COMPLETED.