You are currently exploring our in-stock options for part number 2594484 with the NSN 6605010251271. This product is listed with the description “Transmitter Inducti” and is manufactured by Honeywell International Inc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 2594484 is listed alongside the NSN 6605-01-025-1271 and belongs to the FSC 6605 Navigational Instruments. Additionally, it is also under the CAGE Code 07187, which is assigned to Honeywell International Inc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 2594484 seamless.
MRC | Criteria | Characteristic |
---|---|---|
CRTL | CRITICALITY CODE JUSTIFICATION | SUPP |
AGAV | III END ITEM IDENTIFICATION | BEECH 300 ACFT & CC144 CHALLENGERTRANSPORT ACFT |
SR-5 | DESIGN CONTROL REFERENCE | 2594484 |
SR-5 | THE MANUFACTURERS DATA | |
SR-5 | MANUFACTURERS CODE | 07187 |
FTLD | III FUNCTIONAL DESCRIPTION | THE ""FLUX VALVE"" IS A MAGNETIC AZIMUTH DETECTOR THAT SENSES THE DIRECTION OF THE HORIZONTAL COMPONENT OF THE EARTH'S MAGNETIC FIELD RELATIVE TO THELONGITUDINAL AXIS OF THE ACFT AND CONVERTS INFO TO AN ELECTRICAL SIGNAL WHICH WHEN APPLIED TO THE GYRO,MAINTAINS CONTINUOUS ALIGNMENT TO THE ACTUAL MAG HEADING,RESULTING IN DRIFT-FREE HEADING REFERENCE,SELF-MAINTAINED TO AN ACCURACY OF PORM 2 DEGREES |
SUPP | III SUPPLEMENTARY FEATURES | LOCATED IN A STABLE MAGNETIC LOCATION ON THE ACFT SUCH AS A WING TIP,VERTICAL STABLIZER,OR TAIL CONE;ATTACHEDIS A COMPENSATOR THAT USES MAGNETS TO CANCEL THE SINGLE-CYCLE ERROR CAUSED BY MAGNETIC DISTURBANCES |
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