What was found
#1 ENGINE INLET COWL HAS CORROSION ON BARREL SKIN 1 INCH AFT OF THE INLET LIP AT 12 O'CLOCK POSITION. MARKED<[01] #1 ENGINE INLET COWL REPLACED (FAULT WAS RESOLVED ON ANOTHER FAULT) TTG8Q00S70S4;[02] VERIFIED CORRECTIVE ACTION #1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#1 ENGINE INLET COWL HAS CORROSION ON BARREL SKIN 1 INCH AFT OF THE INLET LIP AT 12 O'CLOCK POSITION. MARKED<[01] #1 ENGINE INLET COWL REPLACED (FAULT WAS RESOLVED ON ANOTHER FAULT) TTG8Q00S70S4;[02] VERIFIED CORRECTIVE ACTION #1