What was found
FUSELAGE OUTER SKIN IS CRACKED AT BULKHEAD FRAME STA 15205 AND STRINGER LT 15. ALSO, STRINGER CROSSOVER CASTALLATION REPAIR ON INTERIOR SIDE IS CRACKED. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE OUTER SKIN IS CRACKED AT BULKHEAD FRAME STA 15205 AND STRINGER LT 15. ALSO, STRINGER CROSSOVER CASTALLATION REPAIR ON INTERIOR SIDE IS CRACKED. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM.