What was found
WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT REAR SPAR, LOWER FWD SCREW HOLE. REPAIRED PER UPS EO DC8-5310-7584-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT REAR SPAR, LOWER FWD SCREW HOLE. REPAIRED PER UPS EO DC8-5310-7584-A.