As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH. SUMMARY OF NRC 00043: FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH WAS REPAIRED PER PRI 606978-14 REV.2 AND ER/A 606978-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-606978 ADDED FOR AC 9551. (LP #2727348)