As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER ERA 626154-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626154-14 REV 3. SEC II ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR, LOG 0961069. (LP #0963096)