As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) BOTH FRAMES CRACKED WHERE THE FLANGE ATTACH RIVETS THAT ARE COMMON TO THE WING TO FUSELAGE CLOSING ANGLES P/N 6511001-49 AND -50 ATTACH. THIS IS THE SECOND A/C WE HAVE FOUND THIS CONDITION ON. A COMPANY GENERATED REPAIR ENGINEERING ORDER WAS USED TO INSTALL REPAIR DOUBLERS. CESCOM SERVICE CONDITION REPORT NR 192167 REFERS. (TC NR 20090114004)