What was found
120AF FLOOR PANEL HAS CORROSION AROUND EDGES. REMOVED CORROSION, ORG MAT .080, MAT LOSS .001, REM MAT .079, FOUND TO BE WITHIN LIMITS 53-0053-1A, ALODINED AND PRIMED IAW SRM 51-20-01-0G. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
120AF FLOOR PANEL HAS CORROSION AROUND EDGES. REMOVED CORROSION, ORG MAT .080, MAT LOSS .001, REM MAT .079, FOUND TO BE WITHIN LIMITS 53-0053-1A, ALODINED AND PRIMED IAW SRM 51-20-01-0G. (K)