You have reached the Request for Quote (RFQ) page for part number 637672, an item sourced from Joint Electronics Type Designation (CAGE Code 80058) that is classified with the item name Computer Aircraft A. Here, you can utilize our online form to quickly secure tailored pricing and procurement options from our staff as the first step of procurement. With responses always being quick, be sure to get started as soon as possible if you would like to learn more about this part number.
Important Details for Part Number 637672
The part number 637672 is associated with Joint Electronics Type Designation, identified by the CAGE Code 80058, and is typically referenced under the item name Computer Aircraft A. It is categorized under the NSN 6605-00-915-9319, with the NIIN 009159319, INC 53058, and NCB code 00 (USA). Additionally, this part falls under the Federal Supply Group (FSG) 66 and Federal Supply Class (FSC) 6605 Navigational Instruments. For more information, these classifications provide further context about the component.
With the form provided, be sure to present our staff with key details on your needs, such as your target pricing, required quantity, and expected turnaround time. Once we receive and review your request for part 637672, a member of our staff will contact you in 15 minutes or less to present customized solutions for your comparisons. Once you make a purchase with us, you can expect our staff to work closely with you through each step of fulfillment to ensure that all needs are met with care and efficiency.
| MRC | Criteria | Characteristic |
|---|---|---|
| MRC | Decoded Requirement | Clear Text Reply |
| AJAF | Unpackaged Unit Length | 23.600 INCHES NOMINAL |
| AJAG | Unpackaged Unit Width | 4.250 INCHES NOMINAL |
| AGAV | End Item Identification | AN/ASN-56 INERTIAL NAVIGATION SYS; RF4C AIRCRAFT |
| RTSE | Relationship To Similar Equipment | REPLACES 6605-00-919-2698 |
| AJAH | Unpackaged Unit Height | 9.740 INCHES NOMINAL |
| FTLD | Functional Description | CONTAINS THE FOLLOW-UP SERVOS FOR PITCH AND ROLL INFORMATION FROM THE INERTIAL NAVIGATION SET STABLE PLATFORM, AND CIRCUITRY FOR COMPUTING VERTICAL ATTACK ANGLE, CLIMB ANGLE, VERTICAL VELOCITY, AND GROUND SPEED TO ALTITDE RATIO |
| AAXX | Mounting Type | BASE, SHOCK MOUNT |
| TMDN | Type/Model Designation | CP-780/ASN-56 |
| AXQK | Output Intelligence Type | ANGLE OF ATTACK |
| AXQJ | Intelligence Input Method | ELECTRICAL |
| AXQH | Input Intelligence Type | ALTITUDE, GENERAL DATA AND GROUND SPEED AND PITCH-ROLL SIGNAL DATA |
| RDAL | Reference Data And Literature | TECH ORDER 5N16-2-6-4 AND DD FORM 61 |
| AWZJ | Power Source | EXTERNAL |
| FEAT | Special Features | ADDITIONAL INFORMATION COMPUTED: CLIMB ANGLE, VERTICAL VELOCITY, GROUND SPEED TO ALTITUDE RATIO |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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