As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INTERGAL PLATE HAS CORROSION AT FRAME 38.2; STRINGER 52R. REMOVED CORROSION PER SRM 51-74-10. FOUND TO BE OUT OF LIMITS PER SRM 53-14-12, FIG 101. FABRICATED REPAIR PARTS PER SRM 53-14-12, REPAIRS 4 & 5. ALODINED PER SRM 51-21-10. PRIMED PER SRM 51-23-10. INSTALLED REPAIR PER A310-200 SRM 53-14-12 REPAIRS 4 AND 5. SEALED PER SRM 51-76-10.