| Mfg Part Number: 8KE89AAD3 | NSN : 6620-01-265-2887 | NIIN : 012652887 |
| CAGE Code : 97424 | Manufacturer: Ametek Inc | Item Name : Converter Signal Data |
| FSC : 6620 Engine Instruments |
Thank you for your continued interest in the parts associated with the NSN 6620-01-265-2887, those of which are readily available for purchase on Automatize Electronics. The Converter Signal Data item associated with the part number 8KE89AAD3, by Ametek Inc, is currently available on our database; thus, if you wish to begin the part number 8KE89AAD3 procurement process, we ask that you please fill out and submit an Instant RFQ form detailing your requirements on parts needed. This includes desired quantities, target prices, expected shipping time frames, and more, as applicable. Upon receival, our representatives will harness your provided information and formulate a solution which satisfies your operational needs in just 15 minutes or less.
With our global supply chain stretching across the United States, Canada, and the United Kingdom, Automatize Electronics can provide expedited shipping on select NSN products with the CAGE Code 97424, strategically assisting entities facing an Aircraft on Ground (AOG) situation or other unique time constraint. Operating with a strict NO CHINA SOURCING pledge, all items are shipped alongside their manufacturer trace documentation or qualifying certifications, ensuring that customers feel confident in every purchase made. With cost savings and rapid lead times bolstering every order, experience all of what Automatize Electronics has to offer on products with the NSN 6620-01-265-2887 by submitting your RFQ for parts by Ametek Inc. submit a quote for the part number 8KE89AAD3, today!
| MRC | Criteria | Characteristic |
|---|---|---|
| BJBP | Connection Type And Location | CONNECTOR, PLUG FRONT |
| FEAT | Special Features | RECIEVES SIGNALS FROM ALL 4 ENGINES, INPUTS OIL PRESSURE, FUEL INLET TEMPERATURE, FUEL FLOW SENSOR (POSITION, SPEED, TORQUER SIGNAL) FAN INLET PRESSURE, FAN DISCHARGE PRESSURE, VIBRATION SIGNAL, TURBINE BLADE TEMPERATURE, FAN SPEED, CORE SPEED, NOZZLE POSITION,OIL TEMPERATURE, OIL QUANTITY;OUTPUTS ARE TO APPROPRIATE INSTRUMENTS, COMPUTORS, FAULT INDICATORS, SEPARATE INPUTS FOR EXHAUST GAS TEMPERATURES (THERMOCOUPLES) OUTPUTS TO AND FROM RIGHT AND LEFT SIDE OSE INTERFACE, INTERNAL FUSE PROTECTED, VARIOUS POWER SUPPLIES FOR CONTROL VOLTAGES (+20, -10, -5, +16, -16, +15 AND +18 VOLTS) |
| FAAZ | Phase | SINGLE |
| MRC | Decoded Requirement | Clear Text Reply |
| AGTA | Basic Shape Style | RECTANGULAR OR SQUARE |
| ABKW | Overall Height | 8.120 INCHES NOMINAL |
| AGAV | End Item Identification | B-1B AIRCRAFT, SIGNAL CONDITIONING AND DISTRIBUTION UNIT |
| ALBM | Operating Control Method | AUTOMATIC |
| ABMK | Overall Width | 8.160 INCHES NOMINAL |
| BHSX | Circuit Construction Type | SOLID STATE |
| ABHP | Overall Length | 18.785 INCHES NOMINAL |
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