Thank you for taking an interest in the NSN 2840-01-459-1286 supplies and listing resources that we provide on Integrated Military Parts. At the top of this page, you will find an overview of NSN 2840-01-459-1286, including details on its associated item name, Federal Supply Group, Federal Supply Class, and more. You can also review a list of all manufacturers that our stock traces back to, each serving as a link to expanded catalogs if you wish to further your search.
Underneath our overview, part numbers like 1559M63, 1559M63G04-118, and others that belong to our NSN 2840-01-459-1286 inventory have been listed out for your perusal. If any are of interest to you, click on the “RFQ” button to its right to access a quote request form. By filling out and submitting a form with detailed information on your requirements and expectations, you will be able to secure fully customized quotes for your comparisons. You can rest assured that you will receive highly competitive options when you shop on Integrated Military Parts, our staff working tirelessly to ensure streamlined fulfillment and satisfaction. Knowing how we intend to serve you, continue perusing solutions on this catalog and reach out as soon as you are ready.
| Item Name | Disk And Hub Compressor Aircraft |
| Federal Supply Group (FSG) | Engines Turbines and Components |
| Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| National Item Identification Number (NIIN) | 01-459-1286 (014591286) |
| NCB Code | USA (01) |
| Manufacturer | General Electric Company, Air Force United States Department |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 1559M63 | general electric company | disk and hub compressor aircraft | 07482 | RFQ |
| 1559M63G04-118 | air force united states department | disk and hub compressor aircraft | 98748 | RFQ |
| 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 |
| Relevant Components for NSN - 2840-01-459-1286, 2840014591286 | ||||
| 2835-01-624-6455 (2835016246455) | 2815-01-307-6161 (2815013076161) | 2825-01-368-7866 (2825013687866) | 2835-01-127-2290 (2835011272290) | |
| 2805-00-407-0607 (2805004070607) | 2815-12-352-8736 (2815123528736) | 2840-00-442-2930 (2840004422930) | 2815-00-404-3615 (2815004043615) | |
| 2835-01-152-6306 (2835011526306) | 2810-00-395-5563 (2810003955563) | 2840-01-216-0188 (2840012160188) | 2825-00-267-3710 (2825002673710) | |
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