What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10, 20 PERCENT CHORD AT 2ND RIVET FROM TOP, 1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-035. 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 IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10, 20 PERCENT CHORD AT 2ND RIVET FROM TOP, 1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-035. MAJOR REPAIR.