What was found
INSPECTION FOUND CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRINGER WAS REMOVED. 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 CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRINGER WAS REMOVED. REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.