As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SECTION 44 WING TO BODY FAIRING SKIN PANEL 192BR HAS ONE LAYER OF CARBON FIBER DELAMINATED UP TO FASTENER HOLE<[01] LENGTH OF DELAMINATION IS 8? X 1.0? AND EXTENDS TO FASTENERS. OUT OF LIMITS PER SRM 53-40-70-1A-1.;[02] COMPLIED WITH EA 25-153-00420 (N8615E- SWA - REPAIR - FUSELAGE SECTION 44 EDGE EROSION AND DELAMINATION TO WING TO BODY FAIRING PANEL 192BR - TIME LIMITED) [TTG8Q00YSJU3]