As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE MAINTENANCE PROCESS THE FRAME 10 INBOARD FLANGE WAS DAMAGED BETWEEN STRINGER 12LH AND STRINGER 13LH. DUE TO IT, A PROPOSED REPAIR LAYOUT HAS BEEN DEVELOPED TO RESTORE THE DAMAGED AREA AND WAS SENT TO EMB FOR APPROVAL. EMB APPROVED THE PROPOSAL REPAIR UNDER THE ETD2026-190-013893 DTD AUG 18 2026 AND DOCUMENTED UNDER COOPESA EO # COO-EO-2026-24878-R00 DTD AUG 18 2026. JOB A1R183 ITEM 2-4