As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(A125-1) AFT CARGO COMPARTMENT; FLOOR STRUCTURE @ DOOR OPENING CORRODED BS792-847; WL156; RBL19-28<[01] REMOVED CORROSION AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED IAW SRM 51-10-02-0G-0VERIFIED LIMITS; ORIGINAL THICKNESS .050'; REMAINIG THICKNESS .026'; MATERIAL LOSS OF .024'; LOSS OF UP TO .005' ALLOWED-OUT OF LIMITS IAW SRM 53-60-15-1A-1 INSTALLED NEW WEB I/A/W BOEING DWG 146A8120 REVA;[02] C/W<BR>AUDIT C/W