As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING INSPECTION CALLED OUT IN AD 2012-18-01, FOUND TWO CRACKS. LT MAIN SPAR AFT FITTING CRACKED IN THE UPPER RADIUS. CRACK LENGTH 1 INCH. RT MAIN SPAR FWD FITTING CRACKED AT INBD BOLT HOLE. CRACK LENGTH .1250 INCH. THE ACFT HAS NO EVIDENCE OF A HARD LANDING.