What was found
PDX C4 - FUSELAGE STRINGER 23L SPLICE ANGLE TOP SIDE HAS CORROSION AT (5) PLACES ON BOTH SLEGS OF ANGLE BETWEEN FUSELAGE STATION X486 - 490. REPAIRED IAW DHC-8-200 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 23L SPLICE ANGLE TOP SIDE HAS CORROSION AT (5) PLACES ON BOTH SLEGS OF ANGLE BETWEEN FUSELAGE STATION X486 - 490. REPAIRED IAW DHC-8-200 SRM 51-40-11.