TRANSDUCER FUEL FLOW/160GPH/ST PICK UP
The transducer is a device that converts the mechanical motion of a spinning turbine into an electronic signal that is read by the fuel computer. The magnetic pick-up assembly detects the spinning turbine and counts the revolutions. This produces a series of pulses that is transmitted to the fuel computer. The computer uses the pulse frequency to calculate the fuel flow over time. The Shadin Avionics Company Incorporated-designed fuel flow transducer can be used in conjunction with all of our fuel totalizer units and fuel/airdata computers.
AeroCorder 100 CVR
iCloth Large Screen and Lens Cleaner | Box of 500
Synchro to ARINC 429 HS Converter
This Synchro to ARINC 429 HS Converter (933800-24) is a general purpose converter, which can be used whenever Synchro to ARINC 429 High speed conversion is required. It can receive three 3-wire Synchro ARINC 407 inputs: pitch, roll and magnetic heading. The received labels are then converted to ARINC 429 high speed. The output labels are: 320 (Magnetic Heading), 324 (Pitch) and 325 (Roll). This converter also receives 3 discreet flag inputs which are used to enable or disable the output of ARINC 429 labels associated with roll (325), pitch (324) and magnetic heading (320).
DC400 Digital DC Fuel Quantity Test Set
The compact and lightweight DC400A is a complete fuel quantity system test set for use on aircraft that have probes with integral diode rectification, commonly called DC fuel quantity systems. Completely self-contained and portable, the DC400A is lightweight and as an internal battery-powered DC fuel quantity system. The tester is specifically designed, when used with the proper Adapter Module, to meet the requirements for testing and calibration of a wide range of Aircraft DC Fuel Quantity Systems.
