The instrument face can be customized according to customer requirements. There can be built-in signalization of V mo. The instrument is manufactured for different speed ranges up to 300 kts ( 600 km/h). The instrument consists of an indicated airspeed pointer and a pointer showing the maximum operating speed of the aircraft ( V mo - set according to customer requirements), which is dependent on barometric altitude. This pressure is indicated in units of airspeed ( kts, mph, km/h). When properly connected to an airspeed tube, mounted so as to be in undisturbed air, the airspeed indicator measures the differential pressure developed between the pitot and static opening. The instrument is intended for use on aircraft to indicate the speed relative to the air at MSL and are used at any other altitude to indicate the equivalent speed corresponding to the actual force of the air. There is also a version with an illuminated instrument face ( supply voltage: 5, 14, 28 VDC - according to customer requirements). Don't hesitate to contact us with your inquiry. There is built-in signalisation of the stall speed of the aircraft. The instrument is manufactured for different speed ranges up to 200 kts ( 400 km/h). The instrument is intended for use on aircraft to indicate the speed relative to the air at MSL and are used at any other altitude to indicate the equivalent speed corresponding to the actual force of the air. There is also a version with an illuminated instrument face ( supply voltage: 5, 14, 28 VDC - according to customer requirements). This instrument fulfills the requirements and methodology rules TSO – C2d and RTCA/DO – 160C. Don't hesitate to contact us with your inquiry.

The instrument is manufactured for different speed ranges up to 300 kts ( 600 km/h).

Airspeed switchies