What was found
FUSELAGE SKIN INNER SURFACE CORRODED IN AVIONICS COMPT ON RIGHT SIDE OF ENTRY HATCH BETWEEN 8 & 9. CORROSION BLENDOUT DEPTH IS BEYOND LIMITS OF SRM 53-10-00. R&R STIFFENER PER EA 6-5330-65-66446.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN INNER SURFACE CORRODED IN AVIONICS COMPT ON RIGHT SIDE OF ENTRY HATCH BETWEEN 8 & 9. CORROSION BLENDOUT DEPTH IS BEYOND LIMITS OF SRM 53-10-00. R&R STIFFENER PER EA 6-5330-65-66446.