What was found
FUSELAGE SKIN INTERNAL & EXTERNAL CORROSION AT LEVEL OF FRAME 24 BETWEEN STRINGERS 19 - 20 RHS. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION IAW EO ATR-53-67-2014.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN INTERNAL & EXTERNAL CORROSION AT LEVEL OF FRAME 24 BETWEEN STRINGERS 19 - 20 RHS. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION IAW EO ATR-53-67-2014.