What was found
PDX - 2 INCH CRACK IN RADIUS OF FORWARD RT WING TO FUSELAGE CONNECTION ANGLE UNDER PULLEYS BRACKET YW23.85X AND X384.500. REPAIRED IAW RD 8-53-5192.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX - 2 INCH CRACK IN RADIUS OF FORWARD RT WING TO FUSELAGE CONNECTION ANGLE UNDER PULLEYS BRACKET YW23.85X AND X384.500. REPAIRED IAW RD 8-53-5192.