As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PER CUSTOMER REQUEST REPLACE THE FASTENER INSTALLED ON CENTER FUSELAGE I, FR26+94MM, STRINGER 11RH+105MM, EXTERNAL SKIN WITH THROUGH DAMAGE REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2018-190-086940 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18985-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-74 ).