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 4085104, a Blade Turbine Rotor Aircraft Gas item that is listed with the NSN 2840-01-445-2811 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 4085104 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 4085104 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 2840-01-445-2811, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. 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 |
---|---|---|---|---|---|---|
2840-01-445-2811 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 014452811 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | 0 | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4085104 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | Diameter | 29.004 INCHES MINIMUM AND 29.404 INCHES MAXIMUM |
CQFM | Hardness Rating | 45.0 ROCKWELL C MINIMUM OVERALL AND 55.0 ROCKWELL C MAXIMUM OVERALL |
MRC | Decoded Requirement | Clear Text Reply |
CZBJ | Engine Section Location | TURBINE |
CRTL | Criticality Code Justification | FEAT AND ABMZ AND ABHP AND CZBJ |
FEAT | Special Features | T.O. 2J-F100-14, FIG 130, IND 9; INTERIM BLADE REPLACES P/N 4067004 AND IS REPLACED BY P/N 4084804 PER ECP 95-NA027 |
CZCJ | Stage Number | 4 |
MDCL | Material Document And Classification | PWA658 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
AGAV | End Item Identification | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
APGF | Design Type | AXIAL COMPRESSOR |
ABHP | Overall Length | 6.771 INCHES MINIMUM AND 6.781 INCHES MAXIMUM |
MATT | Material | NICKEL ALLOY OVERALL |
BGLW | Blade Attachment Method | FIR TREE |
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