As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING AILERON LE UPPER SURFACE AROUND FASTENER HAS 1/4" LONG CRACK PCU AREA. STOP DRILLED CRACK NDT HFEC VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR DOUBLER IAW 57-02-00-0 AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 AND 57-08-00-0. REPAIR DOUBLER CENTERED AT AILERON HINGE LINE "D" VALUE EQUALS ZERO THEREFORE THERE IS NO NET CHANGE IN BALANCE IAW SRM 51-04-08 FIG 59R.