You are currently exploring our in-stock options for part number 53-87012-21-271 with the NSN 6605009159319. This product is listed with the description “Computer Aircraft A” and is manufactured by Boeing Company The. 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 53-87012-21-271 is listed alongside the NSN 6605-00-915-9319 and belongs to the FSC 6605 Navigational Instruments. Additionally, it is also under the CAGE Code 76301, which is assigned to Boeing Company The. 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 53-87012-21-271 seamless.
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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