What was found
RIGHT FUSELAGE AT WING BODY FAIRINGS HAS NUMEROUS SPOTS OF CORROSION AT ATTACHMENT POINTS. FABRICATED DOUBLER, LOCATED, DRILLED PARTS & INSTALLED PERMANENT REPAIR IAW MD80 SRM 51-30-5 & 53-04, PAR 7, FIG 57.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE AT WING BODY FAIRINGS HAS NUMEROUS SPOTS OF CORROSION AT ATTACHMENT POINTS. FABRICATED DOUBLER, LOCATED, DRILLED PARTS & INSTALLED PERMANENT REPAIR IAW MD80 SRM 51-30-5 & 53-04, PAR 7, FIG 57.