As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE HAVING NDT PERFORMED TO COMPLY WITH AD CF-97-07 REV.2, WING TO FUSELAGE FRAME ANGLE INSPECTION, THE LT FRONT OUT BOARD ANGLE WAS FOUND CRACKED. ANGLE WAS REPAIRED IN ACCORDANCE WITH DRAWING 215-53-10-54 PAGES 2,3 & 6. THE AIRCRAFT HAD ACCUMULATED A TOTAL OF 217.2 HOURS SINCE AD WAS LAST DONE.