As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE NDT INSPECTION CRACK WERE FOUND ON THE OTBD FASTENER HOLE LOCATED ON THE FUSELAGE UPPER SKIN NEXT TO BS 727 G (FRONT) AND BETWEEN S2L AND S3L (WHERE AFT SKIN FITTING WAS INSTALLED). PERFORMED REPAIR ON UPER FUESELAGE SKIN 2 INCHES TO FWD FROM BS 727 G BETWEEN S-2L AND S-3L PERFORMED IAW EO260407 P1, EO260407 REV IR. AND EC/RA 5310-08989 REV ORG.