As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT AFT CABIN "R2" DOOR, DOUBLER PLATE ADJACENT TO AND UNDER THE FORWARD GIRT BAR FITTING HAS CORROSION. **AREA MARKED IN RED** GROUNDED - YES. REMOVED CORROSION-ORIGINAL THICKNESS .256 REMAINING .090, REMOVED .166 AND FOUND TO BE OUT OF LIMITS IAW A319 53-41-14. REMOVED AND REPLACED DOOR SILL P/N D5348004320701 IAW A319 SRM 51-42-11 REF AIRBUS DWG# D53480505. THIS IS A CATEGORY "A" REPAIR.