As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SECTION 48 BODY STATION 1809.5 BULK HEAD LH TENSTION FITTING CRACK(<P>REAMED FASTENER HOLE TO A DIAMETER OF 0.3120" AS PER SRM 51-40-05 & SP1-TLS-25-0031-038. PERFORMED OPEN HOLE HFEC INSPECTION PER NDTM 51-00-16 PART 6, RESULT NORMAL. R/R FASTENER PER SRM 51-40-02 & SP1-TLS-25-0031-03B. NO FURTHER DEFECTS NOTED</P>)