As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN LT ENGINE PYLON TOP CUTOUT PANEL NR 5727. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5430-01230. A DIP WAS INITIATED TO REINSPECT THE SKIN AND DOUBLER FOR CRACK GROWTH EVERY 150 FLIGHT CYCLES UNTIL TIP OF CRACK REACHES PRODUCTION FASTENER HOLE.