What was found
#2 ENGINE NOSE COWL LIP SKIN HAS A WORKING FASTENER AT 10 O CLOCK POSITION<[01] #2 ENGINE INLET COWL REPLACED GENERAL FAULT RESOLVED ON OTHER FAULT TTG8Q00S72VD;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#2 ENGINE NOSE COWL LIP SKIN HAS A WORKING FASTENER AT 10 O CLOCK POSITION<[01] #2 ENGINE INLET COWL REPLACED GENERAL FAULT RESOLVED ON OTHER FAULT TTG8Q00S72VD;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.