What was found
PDX C4 - FUSELAGE STRINGER 24L HAS CORROSION AROUND (8) RIVETS ON TOP SIDE, AFT SIDE OF FRAME X510. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX C4 - FUSELAGE STRINGER 24L HAS CORROSION AROUND (8) RIVETS ON TOP SIDE, AFT SIDE OF FRAME X510. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11.