Thank you for taking an interest in our selection of 6605-00-915-9319 parts here on Boost AOG. You are currently on the RFQ form for part number 53-87012-21-271, a Joint Electronics Type Designation System product listed with the Computer Aircraft A If part number 53-87012-21-271 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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To ensure the quality of our NSN components, we adhere to a strict NO CHINA SOURCING pledge, meaning every purchased item will be delivered alongside any pertinent qualifying certifications or manufacturing trace documentation for your benefit. Paired with numerous other commitments, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. If you happen to be facing a time constraint and require NSN parts quickly, contact us at your earliest convenience, and we will discuss the expedited shipping options we have available for domestic and international customers alike. With our various dedications in mind, kick off procurement for Joint Electronics Type Designation System part number 53-87012-21-271 and other Computer Aircraft A products 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 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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