As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, CRACKS WERE DETECTED ON THE NUMBER ONE AND FOUR INBOARD PYLON ATTACH ANGLE STIFFENERS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED ANGLES, FABRICATION AND INSTALLATION OF TWO NEW ANGLES IN ACCORDANCE WITH DOUGLAS DRAWING 5756791 AND ENGINEERING ORDER 54-DC8-919.