The purpose of a control linkage is to take the motion generated by the radio control servos and transfer it to the airplane’s control surfaces and other controll devices. Since this motion is mechanical, there are considerations for choosing one technique versus another. So, in it’s simplest terms, a control linkage will include a servo control arm, push rod, control horn, a way to attach the push rod to the servo control arm and control horn, some way to adjust the position and distance of movement and the controlled device itself. This is obvious to those of us who have been around the R/C circuit for a while, but to the newcomer, this is a challenging topic.
Always plan ahead and avoid mechanical interference between the moving parts. Engine vibration and G-forces will cause our control linkages to behave erratically. These introduce stress and must be considered, even in a docile trainer.
Cost
The real cost of the control linkage is the price of the entire model if it were to fail doing its job! If we take into consideration the initial cost of the hardware, the time it takes to install, adjust, and lock, special tools ,as well as any maintenance during the life of a model, we might want to consider using the higher initial price of carbon fiber push rods (titanium ends give you special bragging rights!), nylon bushed control horns, ball/stud clevises, etc. The old adage “You Get What You Pay For” comes into play here, especially for the Giant Scale and speed models. Many times we use parts because they are part of a kit. We forget that the kit manufacturer makes choices based on their costs – many times providing parts that “will do”, but may not be the best for the application. Some don’t even provide these parts, leaving the choice to the preference of the model builder.
Precision and strength
The important measurement for the control surface is will it provide the proper movement, with no slop, exact mechanical repeatability, no wear, and no maintenance. It must tolerate the stress placed on it during normal reasonable flight. It should tolerate changes in temperature and wear slowly. Parts that have been problematic over time:
Threaded metal clevises that can split apart and/or become stripped by vibration. Sullivan provides an interlocking design that is good.
Nylon parts that are too soft or brittle
Wooden dowels that twist and warp from moisture
Incorrect application or number of supports
Incorrect application (ie. Braided wire for elevators yikes!??)
Size and space
These seem obvious, until considering that each model has many moving parts and these may interfere with each other as they move. Some planning for the elevator