FLAT WASHER

Flat washer for Shadin OAT sensor.

DC Fuel Flow to Frequency Converter

The PSD60-503 Interface combined with a VIAVI Fuel Quantity Test Set provides complete functional testing and troubleshooting of the fuel quantity system.

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KSG 7200: ADAHRS

The KGS 7200 air data attitude heading & reference system (ADAHRS) is a dual channel system that combines attitude, altitude, airspeed, air temperature, and heading information into one unit. This unit utilizes a dual-channel ADAHRS function with state of the art micro-electromechanical sensors (MEMS). Its compact size reduces weight while continuing to provide high reliability for business and general aviation, and civil helicopter markets.

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AeroVue AHRS Install Kit | With 540ft Cable

Attitude Heading Reference System (AHRS) installation kit for the AeroVue Multi-Function Display unit.

Fuel Quantity Test Set Interface | T-Cable, B727, B737, B747

The PSD60-503 Interface combined with a VIAVI Fuel Quantity Test Set provides complete functional testing and troubleshooting of the fuel quantity system.

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Contact Cost Aero at 855-500-3044 for pricing

AeroVue ADAHRS Install Kit

Air Data Attitude Heading Reference System (ADAHRS) installation kit for the AeroVue Multi-Function Display unit.

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A-429 HS/LS TO SERIAL CONVERTER W/SM SEL/OUTPUTS RS-232 or RS-422 SERIAL.

ARINC 429 to RS232 Converter. ARINC 429 High Speed / Low Speed to Serial. Any FMS ARINC output to MX-20 moving map or Electronic Flight Bag.

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Fuel Flow Transducer | Straight Pick-up, 100GPH

The 660535S transducer 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 fuel flow transducer can be used in conjunction with all fuel totalizer units and fuel/air data computers from Shadin.

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Fuel Flow Transducer | 7-160 GPH, Hall Effect, Straight Pick-up

This fuel flow transducer mounts to the engine fuel line and produces electrical signals that represent the fuel flow. The transducer body has hydraulic fittings that connect directly to the engines fuel line, and a small turbine wheel mounted inside with two precision ball bearings driven by the flowing fuel which incorporate a small magnet that is picked-up by a hall-effect sensor. Transducers based on hall effect technology can operate over a broader range of flow rates and in high temperature environments. This transducer also includes an integrated RTD temperature sensor. 

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WASHER/SHOULDER OAT

WASHER/SHOULDER OAT

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KDC 481 Central Air Data Computer | MD900 Helicopter

The KDC 481 is the Centeral Air Data Computer that processes pitot and static pressures and air temperature inputs for the KAD 480 Air Data System. The processed information is supplied to the KCP 420 Flight Computer, KAV 485 Atimeter/Vertical speed indicator, KAI 487 Airspeed indicator, and the KST 488 Speed/Temperature Indicator. Additionally, the KDC 481 supplies the air data necessary for the KAH 460 Altitude Heading Reference System and optional Flight Management Systems.

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Contact Cost Aero at 855-500-3044 for pricing