We are pleased to offer procurement for General Electric Company part number 1559M63 here on NSN Portal, a Disk And Hub Compressor Aircraft product that is listed with the NSN 2840-01-459-1286 for ease of identification. You have reached our Request for Quote (RFQ) form for this listing, where you are encouraged to submit details on your requirements to receive tailored purchasing options from our staff. As you will see, we ask that you offer key information on your pricing target, desired quantity, and more, as this will ensure that the representative who responds to your request is able to provide the most fitting solutions for your needs.
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Whether you procure part number 1559M63 or other NSN products from our website, you can rest assured that we uphold full traceability for all items. For example, this particular listing traces back to General Electric Company through the CAGE Code 07482, as well as falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on having the NSN 2840-01-459-1286. Furthermore, every purchase will be delivered with any applicable qualifying certifications or manufacturer trace documentation as per our NO CHINA SOURCING pledge. If you are ready to experience why professionals rely on us for their needs, request a quote for part number 1559M63 today and take advantage of our industry-leading services.
| 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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