Thank you for your interest in part number CP780ASN56, a component manufactured by Boeing Company The that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 6605-00-915-9319 and features the description “Computer Aircraft A.” To request a quote for part number CP780ASN56, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 6605-00-915-9319 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from Boeing Company The, which is associated with the CAGECode 76301. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 6605 Navigational Instruments part number CP780ASN56.
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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