What was found
FOUND SPANWISE CRACK IN HORIZONTAL STABILIZER LEADING EDGE SKIN BETWEEN STA 98.00 AND STA 103.00. CRACK POSSIBLY CAUSED BY FATIGUE TO THIN SKIN CAUSED BY REPETITIVE REPLACEMENT AND ROLLING DOWN OF EDGES OR STABILIZER DEICER BOOT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND SPANWISE CRACK IN HORIZONTAL STABILIZER LEADING EDGE SKIN BETWEEN STA 98.00 AND STA 103.00. CRACK POSSIBLY CAUSED BY FATIGUE TO THIN SKIN CAUSED BY REPETITIVE REPLACEMENT AND ROLLING DOWN OF EDGES OR STABILIZER DEICER BOOT.