What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE STRINGER ON THE VERTICAL STAB, LT SIDE AT CSS-68 AND 29.75 PERCENT CHORD, HOLE APPROX .5" IN DIAMETER. REPAIRED IAW EO 13-1900-55-019.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE STRINGER ON THE VERTICAL STAB, LT SIDE AT CSS-68 AND 29.75 PERCENT CHORD, HOLE APPROX .5" IN DIAMETER. REPAIRED IAW EO 13-1900-55-019.