What was found
DURING CHECK-C, FOUND FUSELAGE STRINGERS CORRODED AT FS 660 TO 680, S27L TO S27R. REMOVED 3 T ANGLE STIFFENERS, REMOVED CORROSION BY ABRASIVE SANDING AND RE-INSTALLED PER SRM 51-10-6, PG 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C, FOUND FUSELAGE STRINGERS CORRODED AT FS 660 TO 680, S27L TO S27R. REMOVED 3 T ANGLE STIFFENERS, REMOVED CORROSION BY ABRASIVE SANDING AND RE-INSTALLED PER SRM 51-10-6, PG 5.