We appreciate your interest in General Electric Company part number 1559M63, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 1559M63 is listed with the NSN 2840-01-459-1286 and description “Disk And Hub Compressor Aircraft.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by General Electric Company under the CAGE Code 07482 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-01-459-1286 parts and Disk And Hub Compressor Aircraft items your operations require, so request a quote today.
| 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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