From the landing gear/flap operating section of my 14-19 manual:
(All Capital Emphasis is mine.)
"The landing gear and flap operating handles are functional in design and in operation. They are located between the two front passengers on the upright portion of the front seat. To operate, simply grasp the small wheel (to indicate landing gear) or the airfoil section (to indicate flap) and move the handle up or down as you desire the counterpart to move. There will be immediate response as it requires less than two seconds for the entire operation. IT CAN BE STOPPED PARTWAY THROUGH THE CYCLE BY SIMPLY RELEASING THE HANDLE WHICH IS SPRING LOADED AND WILL RETURN TO NEUTRAL LOCKING THE FLUID IN THE LINE AT THAT POSITION. This feature is desirable at times when only part of the entire flap travel is desired. Flap operation time is increased by the installation of a strainer and restrictor in the line. Flaps should not be operated at air speeds above 90 m.p.h. Position of the flap is indicated pictorially by a small mechanical indicator located on the vertical section on the pilot’s left, directly below the instrument panel. It has a wire control connected directly to the flap cylinder. The landing gear should be operated at speeds under 125 m.p.h.
Care must be exercised to prevent inadvertent retraction of the landing gear on the ground. As a precaution against operation by personnel unfamiliar with the ship, it is recommended that the spring-loaded latch which holds the landing gear lever in the down position be engaged. It should be released before starting the engine, for the engine pump will deliver by-pass pressure and foaming of the oil may result. AN IMPORTANT FEATURE OF THIS LATCH IS TO ALLOW SINGLE HAND OPERATION FOR EXTENDING THE LANDING GEAR WHEN USING THE EMERGENCY HANDLE."
Notice that there is no indication that the gear control has a mode that locks the handle down until the gear is fully extended. In fact, there has to be a external, manually operated latch to hold the landing gear lever in the down position - it is not built into the controller.
As far as I know, the 14-19 and 14-19-2 used the same gear/flap controller. The controls are spring loaded to the neutral position and releasing them causes the hydraulic operation to stop.
The -3 may have used a different controller (the same controller as used on the Piper planes), which did have an internal latch that held the gear in the up/down position until the cycle was complete, at which point the internal pressure kicked the control lever back to neutral.
I hope this helps.
Dave