As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSEPCTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #2 HAS CRACKED IN SKIN. WORK ACCOMPLISHED ON FINAL EA #F-5730-T0384448 PT1 MAJOR REPAIR, WINGS-PLATES & SKINS-RH WING UPPER SKIN @ DRAG FITTING CRACK REPAIR-THIS EA DEVIATES FROM EO F- 5730-E0340076.