Thank you for your interest in part number 1559M63, a component manufactured by General Electric Company that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-01-459-1286 and features the description “Disk And Hub Compressor Aircraft.” To request a quote for part number 1559M63, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 2840-01-459-1286 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from General Electric Company, which is associated with the CAGECode 07482. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components part number 1559M63.
| 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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