What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND CRACK IN THE FUSELAGE FRAME IN THE BEND RADIUS AT FS 451 AND STRINGER 10R, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-034. 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 CRACK IN THE FUSELAGE FRAME IN THE BEND RADIUS AT FS 451 AND STRINGER 10R, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-034. MAJOR REPAIR.