As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH. (FUS). SUMMARY OF NRC 00300: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH WAS REPAIRED PER PRI 608247-14 REV 1 AND ER/A 608247-14 REV. ORIGINAL. ACCOMPLISH SECTION II: REPETITIVE INSPECTION WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR IAW ER/A 608247-14 REV ORIG UNDER LP 2786137. (LP #2786331)