As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BULGE ON FUSELAGE SKIN FORWARD OF BS 676 BETWEEN STRINGER S-35L / S-36L.(<P>BULGE WAS REPAIRED AT STA 654+121 / 676 BETWEEN STRINGER S-35 / S-36 IAW <SPAN>SRM 53-00-01-1A-1 </SPAN><SPAN>TRE 6753334 AND FAA FORM 8100-9, REFERENCE ID: 202001150013-000301.</SPAN></P>)