What was found
INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOUBLERS, FINGER DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOUBLERS, FINGER DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.