As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF RT UPPER FUS AFT H/S FAIRING INNER SKIN FWD END HAS A 3 INCH CRACK. CUT OUT DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER IAW DWGD 85350-3. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DWG MMCD 85350-3.