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Quality guaranteed We sell only warrantied and traceable partsIf you have been searching for 1559M63 of Disk And Hub Compre components with NSN 2840014591286 under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, look no further than Limitless Aerospace. 1559M63 part is listed alongside the other Disk And Hub Compre parts, and it has been manufactured by General Electric Inc (CAGE Code 07482). With current availability through our website, we invite you to request a quick and competitive quote for 1559M63 by filling out and submitting the RFQ form below. By providing us with information such as your target price and when you need your parts by, we can ensure that we offer a personalized solution that accommodates your individual needs and requirements.
NSN parts are those that follow the NSN system as dictated by the NATO Standardization Agreements, and they contain a 13-digit serial number to optimize the procurement, stocking, and issuing of items through the federal supply system. On Limitless Aerospace, we make finding the NSN parts and components you need easy, and customers may peruse our robust NSN part catalogues or use our search engine to find specific items with ease. As the only independent distributor with a no China sourcing pledge, we choose to only stock items from top global manufacturers such as General Electric Inc. Get started on the purchasing process for 1559M63 today and see how we can serve as your strategic sourcing partner for all of your operational needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-459-1286 Item Description: Disk And Hub Compre | 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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM |
| ABMZ | DIAMETER | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HPC COMPRESSOR SPOOL |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| 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 | III MATERIAL | TITANIUM ALLOY OVERALL |
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