As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, CORROSION ON CABIN FLOORBEAM AT BS 1050 BLL 65. REMOVED CORROSION PER SRM 51-10-6. ALODINE AND PRIMED CUT OUT DAMAGED AREA PER SRM 51-40-4. FABRICATED ANGLE REPAIR PER SRM 53-10-8, ANGLE SIZE 15 INCHES BY .8750 INCH BY 2 INCHES 7075-T6 0.50 AND 0.80. TOTAL CYCLES 29235.