What was found
CRACK FOUND IN FASTENER HOLE ON LT WING STUB AT CENTRAL FUSELAGE II PRESSURE BULKHEAD TO SPAR III. R & R AN OVERSIZED BUSHING IAW ETD2015-170-041398, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND IN FASTENER HOLE ON LT WING STUB AT CENTRAL FUSELAGE II PRESSURE BULKHEAD TO SPAR III. R & R AN OVERSIZED BUSHING IAW ETD2015-170-041398, REV A.