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 the NSN part 345C-2A. This item was manufactured by Rockwell Collins Inc and is a Accelerometer Elect component with the NSN 6615-01-043-2763. This 345C-2A is available for immediate purchase, and we would be happy to provide you with a quick quotation for your comparisons. To begin, please fill out and submit an Instant RFQ form provided on this page. After receiving your request, an account manager will immediately start crafting a competitive quote that reflects your individual requirements.
Stacked Purchasing offers 345C-2A with various CAGE Code 13499 parts from Rockwell Collins Inc, one of the manufacturers on our thoroughly vetted approved vendor list. Whether it is 6615-01-043-2763 or any other component that we distribute, we stand by the quality of our products. Stacked Purchasing operates with AS9120B, ISO 9001:2015, and FAA AC 00-56B certification and accreditation, and we have an unmatched dedication to providing our customers with the best possible parts. Moreover, our team members take the time to identify customers' exact time requirements, and with our vast distribution network, we are agile in our shipping execution. Please get in touch with our team if you want to learn more about our services. We look forward to being your strategic sourcing partner.
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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