Thank you for considering Boeing Company The part number 53-87012-21, an item we carry that is listed with the NSN 6605-00-915-9319 and product description “Computer Aircraft A.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 53-87012-21 was specifically produced by Boeing Company The under CAGE Code 76301, and with the NSN 6605-00-915-9319, it belongs to FSC 6605 Navigational Instruments. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 53-87012-21 today, knowing we will be in touch shortly after reviewing your information.
| 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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