As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING ACCOMPLISHMENT OF AD CF97-07R2,THE WING TO FUSELAGE FITTINGS WERE BEING INSPECTED IAW SB 215-A476. DURING THE INSPECTION THE RT FORWARD OUTBOARD ANGLE OF THE WING TO FUSELAGE FITTING WAS FOUND CRACKED. THE AIRCRAFT WILL BE REPAIRED IAW MFG REPAIR ENGINEERING ORDER PRIOR TO BEING RETURNED TO SERVICE.