If your operations demand part number 4047224, an item produced by United Technologies Corporation and listed with the description “Hub Compressor Aircraft Gas Turb,” look no further than this page. At your convenience, you can complete the Request for Quote (RFQ) form below with details like your budget, desired quantity, and anticipated fulfillment timeline to receive customized procurement options on part number 4047224. Our representatives will happily treat you to competitive pricing and swift lead times upon their receipt and review of a completed form, regularly responding in 15 minutes or less.
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If you are interested, be sure to explore our website further for related CAGE Code 77445 items or other various products manufactured by United Technologies Corporation. We also present a catalog of all related FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components parts that we currently carry for your perusal. Regardless of what you decide to purchase from us, we will work closely with you to provide dependable, authentic products while ensuring that we address every requirement possible. This being said, get started on requesting quotes for part number 4047224 and any other NSN parts you need on Sky Forge Components to experience our unrivaled fulfillment services.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-033-9081 Item PartTypeName: HUB,COMPRESSOR,AIRCRAFT GAS TURB | 2840 | 010339081 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4047224 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM |
ABMZ | DIAMETER | 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,PLAIN,ROUND |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
CZCJ | STAGE NUMBER | 2 |
FEAT | SPECIAL FEATURES | INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4,FIGURE 115,INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; SEE TCTO 2J-F100(II)-509 SUPERSEDES PN 4036639; F100 FRACTURE CRITICAL PART. |
MATT | MATERIAL | NICKEL ALLOY HUB |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB |
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