What was found
AFTER TAKEOFF THE NR 2 LEADING FLAP STUCK IN THE EXTENDED POSITION. CYCLED FLAPS, NO HELP AND RETURNED TO TPA. WORN INTERNAL ACTUATOR SEALS CAUSED THE NR 2 LEADING EDGE FLAP TO STICK. REPLACED ACTUATOR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER TAKEOFF THE NR 2 LEADING FLAP STUCK IN THE EXTENDED POSITION. CYCLED FLAPS, NO HELP AND RETURNED TO TPA. WORN INTERNAL ACTUATOR SEALS CAUSED THE NR 2 LEADING EDGE FLAP TO STICK. REPLACED ACTUATOR.