What was found
INSPECTION FOUND CORROSION ON CLIP RT SIDE UNDER CABIN FLOOR EIGHT INCHES FORWARD OF FS 1183, STRINGER 18R. FASTENERS AND PARTS WERE REMOVED, A DOUBLER ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND CORROSION ON CLIP RT SIDE UNDER CABIN FLOOR EIGHT INCHES FORWARD OF FS 1183, STRINGER 18R. FASTENERS AND PARTS WERE REMOVED, A DOUBLER ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.