What was found
LEVEL 2 CORROSION, BULGE ON FUSELAGE SKIN LOCATED APROX 24 INCHES UNDER R2 DOOR CENTER LINE. EVALUATED BULGE ON EXTERNAL FUSELAGE SKIN FOUND DAMAGE TO BE EXFOLIATION CORROSION WITH 100% MATERIAL LOSS PERFORMED DAMAGE CUTOUT AND REPAIR AT FR67 AND STGR 31R/H REPAIR DOUBLER WAS CATEGORY B WITH REINSPECTION EVERY 6000 FC FROM FIRST FLIGHT IAW A320 SRM 53-41-11-205-158 AND SRM 53-41-11-300-074 FIGURE 4 REPAIR B INSTALLED DECAL AND CREATED MONITOR AS PER TOPP 30-10- 70 AND PS900-5-1 #4 JOB COMPLETE. (LP: 1636124, AIRCRAFT WAS GROUNDED)