What was found
(CAN) AFTER LANDING FLAP RETRACTION FAILED AT 14 DEGREES. CHANGED RIGHT WING OUTBAORD FLAP INBOARD SCREW JACK ACTUATOR DUE TO HIGH FRICTION. ALSO CHANGED FLAP P.D.U.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) AFTER LANDING FLAP RETRACTION FAILED AT 14 DEGREES. CHANGED RIGHT WING OUTBAORD FLAP INBOARD SCREW JACK ACTUATOR DUE TO HIGH FRICTION. ALSO CHANGED FLAP P.D.U.