We appreciate your interest in Boeing Company The part number CP780ASN56, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number CP780ASN56 is listed with the NSN 6605-00-915-9319 and description “Computer Aircraft A.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Boeing Company The under the CAGE Code 76301 or that similarly fall under the FSC 6605 Navigational Instruments, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 6605-00-915-9319 parts and Computer Aircraft A items your operations require, so request a quote today.
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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