What was found
DURING BEECH TEMP REV INSPECTION, FOUND CRACK APPROX 1 INCH LONG ON FLAP LEADING EDGE. REPAIRED CRACKED IAW AMWA TO 1900-27-00-0001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING BEECH TEMP REV INSPECTION, FOUND CRACK APPROX 1 INCH LONG ON FLAP LEADING EDGE. REPAIRED CRACKED IAW AMWA TO 1900-27-00-0001.