Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number 4082793-01, a Spray Ring Assembly Fuel item that is listed with the NSN 2915-01-439-2368 for an ease of identification. Manufactured by United Technologies Corporation and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number 4082793-01 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number 4082793-01 is manufactured by United Technologies Corporation, it is specifically done so under CAGE Code 77445, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 2915-01-439-2368, one can also determine that this part falls under FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2915-01-439-2368 Item PartTypeName: SPRAY RING ASSEMBLY,FUEL | 2915 | 014392368 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4083223-01 | 6 | 1 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | F100-PW-229 TURBO FAN ENGINE |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MANIFOLD ASSEMBLY |
FEAT | SPECIAL FEATURES | NEW CONFIGURATION PRECLUDES HOT STREAKS AT TWO LOCATIONS WHICH RESULT IN EXCESSIVE AUGMENTOR AFT END DISTRESS/WARPAGE AND FINGER SEAL EROSION |
RDAL | REFERENCE DATA AND LITERATURE | T.O.2J-F100-54,F.53 PENDING;OUTERMANIFOLD,AUGMENTOR,ASSEMBLY OF |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | AIRCRAFT F-15 OR F-16;P/N 4083223-01 IS PRODUCTION CONFIGURATION MAY BEUSED INDISCRIMINATELY WITH P/N 4082793-01 WHICH IS MODIFIED FROM P/N 4075541-01 |
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