As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY CHECK, WING STUB FITTING AT CENTER OF FUSELAGE LL PRESSURE BULKHEAD TO SPAR LLL AROUND FASTENER HOLE RT SIDE. MAINTENANCE REAMED RT SPAR WING STUB FASTENER BORE TO .375 REMOVED ALL DAMAGE IAW SRM 51-41-02. FABRICATED AND DRILLED UP NEW BUSHING FOR REPAIR, REFER TO CONTINUATION CARD VP-031239-2015/564 C1-C2.