Thank you for taking an interest in part number 4082912, a United Technologies Corporation product we have in stock that is listed alongside the NSN 2840014542553 and the description “Duct Augmentor Aircraft Gas Turb.” As part number 4082912 is readily available for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
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To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. For example, part number 4082912 is listed alongside the NSN 2840-01-454-2553, meaning that it also belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Furthermore, this NSN part is specifically manufactured under CAGE Code 77445, a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-454-2553 Item PartTypeName: DUCT,AUGMENTOR,AIRCRAFT GAS TURB | 2840 | 014542553 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | 0 | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4084853 | 1 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | DIAMETER | 45.679 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | F100-229 AIRCRAFT GAS TURBINEE NGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND ABMZ AND FEAT |
CZBJ | ENGINE SECTION LOCATION | AFTERBURNER |
FEAT | SPECIAL FEATURES | AUGMENTOR COMBUSTION CHAMBER DUCT; REPLACES P/N 4073932 AND 4067029 |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F100-24, FIG 92, IND 1 |
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