What was found
INSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.