The Digiflo-L digital fuel management system provides complete fuel management information under real flight conditions without any manual data entry once initial onboard fuel information has been entered. The Digiflo-L...
The AIS-450 Heading Synchro Output is a digital-to-synchro-based converter that receives angular data (heading) on two ARINC 429 inputs and converts it to one ARINC 407 synchro output (3-wire). The...
Shadin’s RemoteFlo is a fuel computer that supplies fuel flow and range ring information to compatible GPS and other aircraft displays or systems eliminating the need for an additional cockpit...
Shadin’s RemoteFlo is a fuel computer that supplies fuel flow and range ring information to compatible GPS and other aircraft displays or systems eliminating the need for an additional cockpit...
The AIS 360 ARINC Buffer/Isolator (EDMO# 833610-02) has two ARINC 429 inputs and two output channels. Labels received on the ARINC 429 low speed input are sent out on the...
The SAC7-35 Airdata Computer for General Aviation is actually four systems in one; it provides an altitude encoder, altitude alerting, fuel flow, and air data computer. SAC 7-35 is an...
Temperature sensor nut compatible with 681201-1 outdoor air temperature (O.A.T.) probe assembly.
The transducer is a device that converts the mechanical motion of aspinning turbine into an electronic signal that is read by the fuelcomputer. The magnetic pick-up assembly detects the spinning...
Shadin Fuel Flow Transducers are the standard in aviation fuel flow meters. Shadin’s broad portfolio of TSO part numbers and installation approvals offer a solution to virtually any aircraft with...
The transducer is a device that converts the mechanical motion of aspinning turbine into an electronic signal that is read by the fuelcomputer. The magnetic pick-up assembly detects the spinning...