As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A 100 HR INSP, (3) CRACKS WERE VISUALLY FOUND IN THE AFT WING SPAR AFT UPPER RADIUS BETWEEN THE LT AND RT IB SEAT TRACKS. ON FURTHER INSP WITH EDDY CURRENT, IT WAS FOUND THAT FWD UPPER RADIUS OF AFT SPAR WAS CRACKED BETWEEN THE LT AND RT IB SEAT TRACKS. TOTAL DAMAGED AREA ON THE FWD AND AFT SIDE OF SPAR IS APPROX 9 INCHES LONG. REPAIR IS BEING DESIGNED BY A DAR AND TO BE COMPLETED.