Link 1 with wheel a turns about fixed axis D of the aircraft frame member. Link 2, provided with a shock absorber, is connected by turning pairs B and C to links 3 and 1. Link 3 turns about fixed axis A of the aircraft frame. Piston rod 5 of retracting cylinder 4 is connected by turning pair E to link 3. Cylinder 4 turns about fixed axis F of the aircraft frame. When piston rod 5 moves into retracting cylinder 4, links 1 and 3 are turned counterclockwise, and the landing gear is retracted as shown by the dash lines.
$1433$LG,AL$