What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND THE VERTICAL STABILIZER RT FWD SPAR CAP ANGLE CRACKED BY TOP RIVET AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO12-1900-55-060. 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 THE VERTICAL STABILIZER RT FWD SPAR CAP ANGLE CRACKED BY TOP RIVET AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO12-1900-55-060. MAJOR REPAIR.