What was found
FUSELAGE FRAME 25 INTERNAL STRAP CORROSION AT STRINGER. CORRODED INTERNAL STRAP PORTION BLENDED OUT & INSPECTED WITHOUT ADDITIONAL FINDINGS FOLLOWING ATR INSTRUCTION IAW EO ATR-53-63-2014.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME 25 INTERNAL STRAP CORROSION AT STRINGER. CORRODED INTERNAL STRAP PORTION BLENDED OUT & INSPECTED WITHOUT ADDITIONAL FINDINGS FOLLOWING ATR INSTRUCTION IAW EO ATR-53-63-2014.