As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER FUSELAGE I, FROM FR33+40MM TO X=11035.0, BETWEEN STRINGER 24LH AND STRINGER 25LH, LOWER EXTERNAL SKIN WITH LIGHTNING STRIKES. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030701 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18927-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-40 ).