What was found
INSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A DOUBLER STRAP REPAIR WAS INSTALLED IAW SRM 53-30-8, 51-10-6, 51-20-4, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A DOUBLER STRAP REPAIR WAS INSTALLED IAW SRM 53-30-8, 51-10-6, 51-20-4, AND 51-30-2.