Thank you for considering United Technologies Corporation part number 4060054, an item we carry that is listed with the NSN 2840-01-205-1303 and product description “Retainer Compressor Vane 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 4060054 was specifically produced by United Technologies Corporation under CAGE Code 77445, and with the NSN 2840-01-205-1303, 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 4060054 today, knowing we will be in touch shortly after reviewing your information.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-205-1303 Item PartTypeName: RETAINER,COMPRESSOR VANE,AIRCRAF | 2840 | 012051303 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4060054 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ADAV | OVERALL DIAMETER | 16.886 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | ACFT ENG F100-PW-220 |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV AND MATT AND ADAV AND FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
FEAT | SPECIAL FEATURES | 4TH STAGE SYNCHRONIZING RING,CASEAND STATOR,DISK & BLADES |
MATT | MATERIAL | ALUMINUM ALLOY |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F100-14; FIG 164,IND 41 |
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