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 III, AT FR90+140MM, STRINGER 27RH+17MM, EXTERNAL SKIN WITH EXISTING THROUGH DAMAGE REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2011-190-06011 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18970-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-53 ).