What was found
INSPECTION FOUND STRINGER 25L CORRODED BETWEEN STRINGER END FITTING FORWARD OF STA 1016. A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, PAGE 206.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND STRINGER 25L CORRODED BETWEEN STRINGER END FITTING FORWARD OF STA 1016. A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, PAGE 206.