What was found
MDT - DURING A SPOT INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED, LEFT AND RIGHT SIDES AT FRAME 4 STRINGER 4. REPAIRS WERE MADE IAW DHC RD8-55-199. AIRCRAFT WAS RETURNED TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MDT - DURING A SPOT INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED, LEFT AND RIGHT SIDES AT FRAME 4 STRINGER 4. REPAIRS WERE MADE IAW DHC RD8-55-199. AIRCRAFT WAS RETURNED TO SERVICE.