As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE. SUMMARY OF NRC 00056: FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE WAS REPAIRED PER PRI 626216-14 REV 1 AND ER/A 626216-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0964238)