As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PER CUSTOMER REQUEST RE-CONTOUR THE SKIN AREA LOCATED AT CENTER FUSELAGE III, BETWEEN FR78 AND FR80 AND BETWEEN STRINGER 2RH AND STRINGER 6RH TO COMPLY WITH THE DISPOSITION OF THE ETD2014-008066. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2014-190-008066 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2024-19201-R00 ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N232 ITEM 21-56 ).