What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE FROM UPPER FASTENER HOLE TO UPPER EDGE OF ANGLE, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-050. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE FROM UPPER FASTENER HOLE TO UPPER EDGE OF ANGLE, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-050. MAJOR REPAIR.