Mfg Part Number: 345C-2A | Alternate P/N: 345C2A |
NSN : 6615-01-043-2763 | NIIN : 010432763 |
CAGE Code : 13499 | Manufacturer: Rockwell Collins Inc |
Item Name : Accelerometer Elect | FSC : 6615 Automatic Pilot Mechanisms and Airborne Gyro Components |
Thank you for your interest in acquiring NSN parts and components from Stacked Hardware. NSN 6615-01-043-2763 is listed alongside the part number 345C-2A, having been manufactured by Rockwell Collins Inc. If you would like to purchase this part or any other specialized items related to Accelerometer Elect from our catalog, we invite you to complete and submit an RFQ form as provided below for part 345C-2A. Upon completing the form, we ask that you provide as many details as you can about the parts or components you wish to procure such as target prices, desired quantities, and expected shipping time frames. With such information, our team of dedicated account managers can draft a solution that keeps your unique requirements in mind.
The particular Rockwell Collins Inc part like 345C-2A you wish to purchase was produced under CAGE Code 13499. The quality of our offerings is guaranteed by our strict NO CHINA SOURCING pledge and the countless quality assurance measures our items are subject to prior to shipping out to our customers. We proudly operate as an AS9120B, ISO 9001:2015, and FAA AC 00-56B certified enterprise, ensuring that you are getting exactly what you need when you need it. Complete an RFQ form today for NSN 6615-01-043-2763 or contact one of our dedicated representatives to see how Stacked Hardware can help you with all your operational needs.
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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