As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING FLAP INSPECTION FOUND THE FLAP FITTING (THE THICK STYLE) TO BE CRACKED APPROX 5 INCHES ON ONE SIDE AND 8 INCHES ON THE OTHER, AND THE FLAP HINGE TO ALSO BE CRACKED AT THE AFT BOLT ATTACHMENT POINT WING STATION 123.38. INSPECTED CRACK BY DYE PENETRANT INSPECTION METHOD IAW SAAB NDI MANUAL 51-08-00, NO CRACK FOUND.