What was found
C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STIFFENER ASSEMBLY AT FR12+4.0 INCHES, -Y1292. REPLACED STIFFENER ASSEMBLY AT FR12+4.0 INCHES, -Y1292 IAW A319 SRM 51-42-11, PAR 5, FIG 10A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STIFFENER ASSEMBLY AT FR12+4.0 INCHES, -Y1292. REPLACED STIFFENER ASSEMBLY AT FR12+4.0 INCHES, -Y1292 IAW A319 SRM 51-42-11, PAR 5, FIG 10A.