Removed in working order from a Stemme S12 as part of a panel upgrade.
Roughly half the price of a new instrument.
Airspeed indicators measure the difference between total pressure and static pressure. The total (or measured) pressure is sensed by a pitot tube positioned at the stagnation point of the airstream and is carried to the airspeed indicator by a hose. A static pressure sensor can also be connected.The measuring element is an open diaphragm unit with excellent elastic properties; hysteresis (differences between advance and return movement) and secondary elastic effects are negligible. The effect total pressure and static pressure acts on the diaphragm, causing a deformation, that is transferred to the pointer by a linkage and gear mechanism.
Operating ranges of your aircraft will need to be identified by custom colour markings on the airspeed indicator dial (not included).