As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND RT WING STUB AT CENTRAL FUSELAGE II PRESSURE BULKHEAD TO WING SPAR III FASTENER HOLE SHOWING CRACKS INDICATIONS X= 15814, OVERSIZED THE FASTENER HOLE BY REAMING FROM .311" TO .341" TO REMOVE CRACKS. INSTALLED BUSHING IAW SB 170-57-0038.