As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN EDDY CURRENT INSPECTION REQUIRED PER AD 2017-10-01, A CRACK WAS FOUND IN THE BEND BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT SIDE OF FRAME 33. CRACK IS LOCATED BETWEEN STRINGERS 5L AND 6L AND IS APPROXIMATELY .75 INCHES LONG. CRACKS TO BE REPAIRED PER DASSAULT FALCON ENGINEERING WITH DOA APPROVAL.