As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER WING FRONT SPAR; UPPER LEFT FISH PLATE HAS A CRACK INDICATION AT THE FWD, UPPER INBD HOLE COMMON TO THE SPAR. REMOVED FITTING REF A310-200 SRM 51-40-21, PG 7. ACCOMPLISHED BHEC ON HOLES REF NTM 57-10-25 PART 6. REMOVED AND INSTALLED 4 FASTENERS ON THE SIDE OF THE FUSELAGE; 2 LEFT SIDE AND 2 RIGHT SIDE FOR ACCESS REF A310-200 SRM 51-40-21; PG 7. REAMED HOLE, FABRICATED AND INSTALLED REPAIR BUSHINGS AND 1 FASTENER REF EA 6-5710-127901