What was found
DURING THE STRUCTURAL INSPECTION IT WAS FOUND AT ENGINE #1 AIR INLET MODULE, OUTER BARREL UPPER PANEL, SKIN WITH REPAIR WITHOUT RECORDS, THE REPAIR WAS REMOVED AND BLEND OUT WAS FOUND OUT ALLOWABLE DAMAGE LIMITS AS PER SRM 71-61-01 AD52 AND A REPAIR WAS INSTALLED AS PER E.O. # COO-EO-2022-15054-R00- WO A1K181 ÍTEM 21-80, APPROVED ON FAA FORM 8110-3 PROVIDED BY A DER.