What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT VERTICAL FWD SPAR CAP ANGLE HAS A CRACK AT TWO RIVETS AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-059. 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 LT VERTICAL FWD SPAR CAP ANGLE HAS A CRACK AT TWO RIVETS AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-059. MAJOR REPAIR.