Thank you for your interest in Boeing Company The part number 637672, a Computer Aircraft A item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 6605-00-915-9319, and you can obtain customized procurement solutions on this component from our team members by completing and submitting the form below. For our specialists to best deliver quotes that accommodate your specifications, please be sure we are presented with essential details like your target price, desired quantity, and anticipated fulfillment timeline. Once we have the opportunity to receive and review your submission, we will strive to provide a tailored response for your consideration within 15 minutes or less.
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Besides part number 637672, you may browse our platform further for similar components produced by Boeing Company The under the CAGECode 76301, as well as additional products that are categorized under FSC 6605 Navigational Instruments. If you have any questions regarding our services or the NSN 6605-00-915-9319 items that we sell, you may always give us a call or email, as we would be delighted to assist you in any way that we can. Otherwise, we encourage you to request a quote for part number 637672 at your earliest convenience.
| 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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