As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(6-5710-T0307446 B PT4) L/H REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE / FRAME 47 FASTENER HOLE "G" HAS CRACK INDICATION NOTED AT 12:0'CLOCK BOTTOM LAYERS. REPAIRED FASTENER HOLE "G" PER EA T-6-5710-T0307446 C PT8 WINGS - BASIC WING STRUCTURE - AD 2019-12-04 - REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE / FRAME 47 FASTENER HOLES "A" (LHS AND RHS). MAJOR REPAIR