Thank you for choosing to partner with National Stock Number Shop for the Disk And Hub Compressor Aircraft NSN parts you require. On this page, you can submit a quote request for General Electric Company part number 1559M63, a component that can also be found by inputting NSN 2840014591286 in our search engine. Apart from this item, we also have an array of other in-demand part numbers, all of which can be traced back to a conglomerate of well-known manufacturers that we trust. Explore our expansive part catalogs by scrolling over to our menu and locate products according to manufacturer, NIIN, NSN, and more.
National Stock Number Shop works with numerous government and defense agencies, so we use CAGE Codes like 07482 to uniquely identify items in a standardized manner. Additionally, we utilize Federal Supply Classes (FSCs) to organize our stock, ensuring customers can find General Electric Company parts under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease. With this in mind, we encourage you to complete the RFQ form below for NSN 2840014591286 or any others, and see how we can provide you with a customized sourcing solution. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock for customer inquiries!
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-459-1286 Item PartTypeName: DISK AND HUB,COMPRESSOR,AIRCRAFT | 2840 | 014591286 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559M63 | 5 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | Diameter | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM |
FEAT | Special Features | PT.O. 2J-F110-4, FIG 67, IND 5; HPCR STG 1-2, SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE; CAN ONLY BE USED ON THE F118-GE-100 AIRCRAFT JET TURBINE ENGINE |
MATT | Material | TITANIUM ALLOY OVERALL |
MRC | Decoded Requirement | Clear Text Reply |
CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME HPC COMPRESSOR SPOOL |
AGAV | End Item Identification | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
CZBJ | Engine Section Location | COMPRESSOR |
ABHP | Overall Length | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM |
APGF | Design Type | AXIAL COMPRESSOR |
CRTL | Criticality Code Justification | ABHP AND ABMZ AND FEAT |
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