What was found
RT WING STUB AT CENTER FUSELAGE II PRESSURE BULKHEAD TO SPAR III FASTENER HOLE CRACKED. HOLE REAMED TO .372" TO REMOVE CRACK, FAB AND INSTALLED OVERSIZED BUSHINGS EAW ETD2015-170-015818, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING STUB AT CENTER FUSELAGE II PRESSURE BULKHEAD TO SPAR III FASTENER HOLE CRACKED. HOLE REAMED TO .372" TO REMOVE CRACK, FAB AND INSTALLED OVERSIZED BUSHINGS EAW ETD2015-170-015818, REV A.