Thank you for considering United Technologies Corporation part number 4077877-02, an item we carry that is listed with the NSN 2840-01-368-6493 and product description “Vane Assembly Compressor Aircraf.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 4077877-02 was specifically produced by United Technologies Corporation under CAGE Code 77445, and with the NSN 2840-01-368-6493, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 4077877-02 today, knowing we will be in touch shortly after reviewing your information.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-368-6493 Item PartTypeName: VANE ASSEMBLY,COMPRESSOR,AIRCRAF | 2840 | 013686493 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4083877-02 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
FEAT | SPECIAL FEATURES | NE NAME TO BE VANE SEGMENT,COMPRESSOR,TURBINE ENGINE; NO. OF VANES IN SEGMENT IS APPROX 10 |
MATT | MATERIAL | NICKEL ALLOY VANE |
RDAL | REFERENCE DATA AND LITERATURE | T.O.2J-F100-54 F96 I81 |
ABHP | OVERALL LENGTH | 3.327 INCHES MINIMUM AND 3.341 INCHES MAXIMUM |
ABMZ | DIAMETER | 24.401 INCHES MINIMUM AND 24.405 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
CZCJ | STAGE NUMBER | 7 |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
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