As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C FX SKIN LAP S39L OUTER SKIN 1EA TOP ROW FASTENER LOCATION AT BS 789 FOUND MATERIAL LOSS APPROX 0.012" ( IE > 10% ), FUSELAGE OVERLAPPING SKIN REPAIRED AT BS 782-795 S38L - S39L AREA AS PER SRM 53-30-03 FIG 11 WITHOUT ZERO TIMING AT CRITICAL ROW FASTENER SUBSEQUENT INSP ARE NECESSARY FOR CATEGORY B REPAIR REFER TO TABLE II INTERNAL HFEC AT 6000 CYCLE IS RECOMMENDED