What was found
DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN OIL CANNED BETWEEN BS446, BS460 ABOVE STR 19 LT. REF FASI NR 86517, CUT OUT DAMAGED AREA DIM 7.5 X 3.375. INSTALLED REPAIR IAW FVCI DWG NR 53-04396-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN OIL CANNED BETWEEN BS446, BS460 ABOVE STR 19 LT. REF FASI NR 86517, CUT OUT DAMAGED AREA DIM 7.5 X 3.375. INSTALLED REPAIR IAW FVCI DWG NR 53-04396-1.