What was found
LEVEL 2 CORROSION, LEFT OF AFT FUSELAGE IS CRACKED BETWEEN FS 1585 AND FS 1605L, LONGERON 25L. CUTOUT DAMAGED AREA, TREATED AND PRIMED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 2 CORROSION, LEFT OF AFT FUSELAGE IS CRACKED BETWEEN FS 1585 AND FS 1605L, LONGERON 25L. CUTOUT DAMAGED AREA, TREATED AND PRIMED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00. (W)