| Mfg Part Number: 345C-2A | Alternate P/N: 345C2A |
| Manufacturer: Rockwell Collins Inc | NSN : 6615-01-043-2763 |
| NIIN : 010432763 | Item Name : accelerometer elect |
| CAGE Code : 13499 | FSC : 6615 Automatic Pilot Mechanisms and Airborne Gyro Components |
Thank you for your interest in our available 345C-2A NSN part. This part number 345C-2A is a Accelerometer Elect listed under the FSC 6615 Automatic Pilot Mechanisms and Airborne Gyro Components, and it is manufactured by Rockwell Collins Inc. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of 345C-2A NSN component, and we carry recently requested NSN components such as 6615010432763. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as Rockwell Collins Inc. If you are interested in this particular item, we invite you to begin the purchasing process for 345C-2A today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | Overall Height | 4.000 INCHES NOMINAL |
| ABMK | Overall Width | 3.500 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| AGAV | End Item Identification | C130H AIRCRAFT |
| FEAT | Special Features | ELECTROSTATIC SENSITIVE DEVICE; INPUT POWER REQUIREMENTS 26VAC 400HZ SINGLE PHASE; MFG NAME SCCELERATION SENSOR; CASE MATERIAL ALUMINUM; UNIT PROVIDES ACCELERATION SIGNALS TO FLIGHT DIRECTOR AND AUTOPILOT SYSTEMS. IT SENSES A CHANGE IN NORMAL FLIGHT ACCELERATION AND GENERATES A PROPORTIONAL SIGNAL. ALSO PROVIDES A MONITOR SIGNAL WHICH INDICATES RELIABLE OPERATION OF THE UNIT. AIR FORCE TECH ORDER 5A22-2-6-3 |
| BGNN | Gravity Unit Range | -1 |
| ABHP | Overall Length | 3.500 INCHES NOMINAL |
| ALGC | Mounting Configuration | 4 MOUNTING HOLES ON BASE |
| CRTL | Criticality Code Justification | FEAT |
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