As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H INBOARD MAIN FLAP DELAMINATED AT TRAILING EDGE DELAMINATION IS 22.5 LENGTH 9.5 WIDTH 3.5 INCHES FROM OUTBOARD EDGE OF LH INBOARD MAIN FLAP<[01] COMPLIED WITH EA 25-157-00209. REINSPECT DUE EVERYDAY 8 DAYS WITH PERMANENT REPAIR DUE WITHIN 131 DAYS. REF FAULT TTG8Q00YD6P9 FOR ENGINEERING AUTHORIZATION DETAILS.