As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SAL - DURING C8 CHECK DISCOVERED CRACK IN THE NR 52, 54 AND 55 HOLES OF THE LT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVERSIZING THE HOLES BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 52, 54 AND 55 HOLES OF THE LT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5721-05153-ES1.