As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - C1 - MAJOR REPAIR - CRACK IN NR 2 ENGINE NACELLE STRUT AT 7 O'CLOCK POSITION IN ALUMINUM CHORD IN OUTBOARD AFT HINGE FITTING UPPER AFT FASTENER HOLE. REPAIRED NR 2 ENGINE NACELLE STRUT OUTBOARD AFT HINGE FITTING UPPER AFT FASTENER HOLE IAW US AIRWAYS EA 100950.