Whether you are in need of military aviation parts, NSN components, or various forms of aerospace and defense parts, Aerospace Store is a single-sourcing solution with over 2 billion product listings readily available for purchase at any time with competitive pricing. You have reached the Request for Quote (RFQ) page for part number 710411, a United Technologies component we feature that is listed with the NSN 2840009294378 and item name “Hub Compressor Aircraft Gas Turb.” For further identification, part number 710411 was also specifically produced under CAGE Code 77445 and belongs to Federal Supply Class (FSC) 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. If you would like to receive specific options for procurement that have been tailored to your unique needs and restrictions alike, we ask that you please fill out and submit the form provided on this page with as much information as you can. Once our team has a chance to receive and review your offered details, a dedicated account manager will be in touch shortly after.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-929-4378 Item Description: Hub Compressor Aircraft Gas Turb | 2840 | 009294378 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | isc | rnvc | rncc | HCC | MSDS | SADC |
710411 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 16.500 INCHES MINIMUM AND 16.570 INCHES MAXIMUM" |
ABMZ | DIAMETER | 18.740 INCHES MINIMUM AND 18.760 INCHES MAXIMUM" |
AGAV | END ITEM IDENTIFICATION | ENGINE MODEL TF33" |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV" |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR" |
FEAT | SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE" |
MATT | III MATERIAL | NICKEL ALLOY OVERALL" |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" |
ABHP | OVERALL LENGTH | 16.500 INCHES MINIMUM AND 16.570 INCHES MAXIMUM" |
ABMZ | DIAMETER | 18.740 INCHES MINIMUM AND 18.760 INCHES MAXIMUM" |
AGAV | END ITEM IDENTIFICATION | ENGINE MODEL TF33" |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV" |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR" |
FEAT | SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE" |
MATT | III MATERIAL | NICKEL ALLOY OVERALL" |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" |
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