What was found
FLOORBEAM 38 CORRODED. FLOORBEAM 38 CORROSION REMOVED IAW SRM 51-21-42 AND IT IS WITHIN AS PER SRM 53-61-00 FIG 301. MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FLOORBEAM 38 CORRODED. FLOORBEAM 38 CORROSION REMOVED IAW SRM 51-21-42 AND IT IS WITHIN AS PER SRM 53-61-00 FIG 301. MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301.