What was found
DURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FWD FUSELAGE FUSE WET AREA, CORROSION FOUND ON RT, INBD SEAT TRACK, MULTIPLE SPOTS, REPLACED IAW SRM 51-41-02 AND SRM 51-43-03. REV 50. CORROSION LEVEL 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FWD FUSELAGE FUSE WET AREA, CORROSION FOUND ON RT, INBD SEAT TRACK, MULTIPLE SPOTS, REPLACED IAW SRM 51-41-02 AND SRM 51-43-03. REV 50. CORROSION LEVEL 2.