What was found
C4 PDX - LEFT OUTBOARD AFT WING TO FUSELAGE CLOSING ANGLE IS CRACKED AT LAST 2 OUTBOARD HILOCKS. REPAIRED IAW RD8-53-5192.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C4 PDX - LEFT OUTBOARD AFT WING TO FUSELAGE CLOSING ANGLE IS CRACKED AT LAST 2 OUTBOARD HILOCKS. REPAIRED IAW RD8-53-5192.