As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, FUSELAGE FRAME 1166 STRINGER 17R HEAVY CORROSION. REMOVED FASTENERS AS PER SRM 51-30-2. CUT OUT DAMAGE AREA AS PER SRM 51-40-3. FABRICATED FRAME REPAIR AS PER SRM 51-40-3 MATERIAL 7075-T6 ,090 11 INCH BY 1 INCH BY 9 INCH FILLER 7075-T6 .100 11 INCH BY 1 INCH BY 19 INCH DOUBLER. INSTALLED FRAME REPAIR AS PER SRM 51-40-3.