What was found
DURING SCHEDULED HC2 CHECK, FOUND CRACK IN FUSELAGE AT STA 500D +14, STR 16L, ONE INCH FROM UNDER SKIN DOUBLER. REPAIR SKIN PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED HC2 CHECK, FOUND CRACK IN FUSELAGE AT STA 500D +14, STR 16L, ONE INCH FROM UNDER SKIN DOUBLER. REPAIR SKIN PER SRM.