As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD CABIN FLOOR SUPPORT BEAM +Y254 BETWEEN FR 16 AND FR 20 CORRODED IN SEVERAL AREAS. REMOVED CORROSION IAW A319 SRM 51-74-00. AFTER REWORK DIMENSION LENGTH 2.5" WIDTH 2.0" DEPTH .075" ORIGINAL MATERIAL THICKNESS .150". FOUND OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 104 ITEM 3. REMOVED AND REPLACED FLOOR SUPPORT AT +Y254 FROM FRAME 24 IAW A319 SRM 51-42-11. STRINGER 490428 BFM