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Page Title: Nose gear up cycle schematic.
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LANDING  GEAR  SYSTEMS OPERATION
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Aviation Structural Mechanic (H&S) 3&2 - How airplanes are built and how to maintain them
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EMERGENCY  SYSTEMS

Figure 12-2.–Nose gear up cycle schematic. When the landing gear handle is in the UP position, a circuit is completed from the landing gear handle circuit breaker, through the landing gear up switch, to the  selector  valve.  The  selector  valve  is  electrically positioned  to  direct  pressure  into  the  landing  gear  up lines and to vent the down lines to return. Fluid flows from the selector valve, through a flow reguIator to the up  side  of  the  nose  gear  cylinder.  Fluid  also  flows through  another  flow  regulator  to  the  down  lock cylinder.  The  down  lock  cylinder  disengages  the  down lock, and the nose gear cylinder starts to raise the nose gear. As the gear is raised, the nose gear doors are closed by mechanical linkage. When the gear is fully retracted, the up lock mechanism engages the nose gear to lock it in  the  up  position.  The  up  lock  mechanism  is mechanically actuated through linkage connected to the nose gear. As soon as the down lock mechanism is disengaged and the gear starts to retract, the pilot’s position indicator displays change from a wheel to a barber pole, and the transition light on the landing gear control panel comes on. As soon as the gear is up and locked, the transition 12-3

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