As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 CRACK IN SKIN WITH CORROSION AT FASTENER ON RIGHT HAND SIDE OF NR 2 ENGINE COWL, STA 2120 UPPER SURFACE AT BASE OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5530-01179. THE CORROSION WAS REMOVED IAW SRM 51-21-01.