You have reached the Request for Quote (RFQ) page for part number DAA3271A003-003, an item sourced from The Boeing Company (CAGE Code 81205) that is classified with the item name Control Unit Pump. Here, you can utilize our online form to quickly secure tailored pricing and procurement options from our staff as the first step of procurement. With responses always being quick, be sure to get started as soon as possible if you would like to learn more about this part number.
Important Details for Part Number DAA3271A003-003
The part number DAA3271A003-003 is associated with The Boeing Company, identified by the CAGE Code 81205, and is typically referenced under the item name Control Unit Pump. It is categorized under the NSN 2915-01-440-3488, with the NIIN 014403488, INC 46631, and NCB code 01 (USA). Additionally, this part falls under the Federal Supply Group (FSG) 29 and Federal Supply Class (FSC) 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. For more information, these classifications provide further context about the component.
With the form provided, be sure to present our staff with key details on your needs, such as your target pricing, required quantity, and expected turnaround time. Once we receive and review your request for part DAA3271A003-003, a member of our staff will contact you in 15 minutes or less to present customized solutions for your comparisons. Once you make a purchase with us, you can expect our staff to work closely with you through each step of fulfillment to ensure that all needs are met with care and efficiency.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2915-01-440-3488 Item Description: CONTROL UNIT,PUMP | 2915 | 014403488 | 666192.32 | N | N | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
0 | PUMP | A | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
DAA3271A003-003 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | PACER SPECIAL |
NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | AN INTEGRATED SYSTEM COMBINING FUEL QUANTITY MEASUREMENT ,FUEL CENTER OFGRAVITY COMPUTATION ,FUEL TANK TEMPERATURE ,AND ENGINE INLET FUEL TEMPERATURE MEASUREMENT;AS FUEL IS CONSUMED AND PUMPED TO THE ENGINE ,THIS COMPUTER ANALYZES VARIOUS DATA |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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