What was found
AFT BILGE LOWER FUSELAGE FRAME UPPER CHORD STRAP IS CORRODED AT STA 1810, RBL 61 AROUND C-2 DOOR OPENING AREA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT BILGE LOWER FUSELAGE FRAME UPPER CHORD STRAP IS CORRODED AT STA 1810, RBL 61 AROUND C-2 DOOR OPENING AREA.