Aerospace Performance Parts is pleased to offer immediate purchasing options for Boeing Company The part number 53-87012-21, which you have taken interest in. This Computer Aircraft A item is listed alongside the NSN 6605-00-915-9319 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 53-87012-21 or any other FSC 6605 Navigational Instruments components we carry from Boeing Company The under CAGE Code 76301, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 6605-00-915-9319 part number 53-87012-21 today, knowing we will support all your operational needs with care.
| 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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